a 320321 mel cdl

7/23/2019 A 320321 Mel Cdl

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SAUDI ARABIAN AIRLINES

MEL

/

CDL

A‐320

A‐321

7/23/2019 A 320321 Mel Cdl


NUMBER DATE CHANGED INITI AL NUMBER DATE CHANGED INITI AL NUMBER DATE CHANGED INITI AL

1 36 71

2 37 72

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5 40 75

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8 43 78

9 44 79

10 45 80

11 46 81

12 47 82

13 48 83

14 49 84

15 50 85

16 51 86

17 52 87

18 53 88

19 54 89

20 55 90

21 56 91

22 57 92

23 58 93

24 59 94

25 60 95

26 61 96

27 62 97

28 63 98

29 64 99

30 65 100

31 66 101

32 67 102

33 68 103

34 69 104

35 70 105

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LOG OF REVISIONS

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MEL/CDLMEL/CDL MANUAL

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INTRODUCTION

A. Approval

The A 320 / 321 MEL/CDL Manual has been developed using thefollowing documents:

1) FAA 320/321 Master Minimum Equipment List (MMEL), Revision 22.

2) Airbus 320/321 Master Minimum Equipment List (MMEL), Date 31 JAN 12.

3) A 320/321 Airplane Flight Manual, Appendix CDL, Date 21 FEB 12.

General Authority of Civil Aviation Approval

Approved By:

Director Flight Operations Signature & Date

Safety & Economic Regulation

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CONTEN

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B. MEL/CDL MANUAL CONTENTS AND ORGANIZATION

This Manual is divided into four Sections as detailed below:

Section 00 – Table of Contents, Introduction, Log of Revisions, and Control Page.

Section 01 – EICAS CROSS-REFERENCE LIST and MEL and (O) PROCEDURES.

This Section consists of MEL Table of Contents, Preamble, Definitions, EICAS Cross-Reference List

introduction, EICAS Cross-References, MEL and Operating (O) procedures.

Section 02 – CDL.

This Section consists of CDL Table of Contents, CDL Item General Locations, Notes, and CDL.

Section 03 – MEL (M) Procedures.

This section has been removed as per the Airbus MMEL new format and replaced with AircraftMaintenance Manual (AMM), this reference is only for maintenance personnel to follow.

Page Numbering:

The MEL, CDL, and Maintenance Procedures pages are numbered as follows:

01.21.01

Assigned Page Number

02.21.01

ATA System Number

03.21.01

Section Number

* * *

00.01.02CONTENTS

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ATA NUMBER SYSTEM PAGE

TABLE OF CONTENTS

- - LOG OF REVISIONS.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.00.01 THRU 00.00.0- - INTTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.01.01 THRU 00.01.0

- - MEL/CDL MANUAL TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . 00.02.01 THRU 00.02.0

- - LIST OF EFFECTIVE PAGES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.03.01 THRU 00.03.2

MINIMUM EQUIPMENT LIST - SECTION 01

- - MEL TABLE OF CONTENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.00.01 THRU 01.00.2

- - FAA MMEL PREAMBLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.01 THRU 01.01.0

- - DEFINITIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.02 THRU 01.01.0

- - ECAM WARNING GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.02.01 THRU 01.02.0

- - ECAM WARNING LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.03.01 THRU 01.03.2

21 AIR CONDITIONING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.01 THRU 01.21.5

22 AUTO FLIGHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01 THRU 01.22.2

23 COMMUNICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.01 THRU 01.23.2

24 ELECTRICAL POWER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.01 THRU 01.24.2

25 EQUIPMENT/FURNISHINGS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.01 THRU 01.25.2

26 FIRE PROTECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01 THRU 01.26.2

27 FLIGHT CONTROLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.01 THRU 01.27.5

28 FUEL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01 THRU 01.28.6

29 HYDRAULIC POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.01 THRU 01.29.2

30 ICE AND RAIN PROTECTION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.01 THRU 01.30.2

31 INDICATING / RECORDING SYSTEMS . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.01 THRU 01.31.2

32 LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.01 THRU 01.32.5

33 LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.01 THRU 01.33.1

34 NAVIGATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01 THRU 01.34.3

35 OXYGEN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.01 THRU 01.35.0

36 PNEUMATIC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01 THRU 01.36.1

38 WATER & WASTE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.38.01 THRU 01.38.0

46 INFORMATION SYSTEM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.01 THRU 01.46.0

47 INERT GAS SYSTEM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.47.01 THRU 01.47.0

49 AIRBORNE AUXILIARY POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.01 THRU 01.49.0

52 DOORS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.01 THRU 01.52.3

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56 WINDOWS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.01 THRU 01.56.04

70 ENGINE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.01 THRU 01.70.02

73 ENGINE FUEL AND CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.01 THRU 01.73.04

74 IGNITION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.01 THRU 01.74.04

76 ENGINE CONTROLS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.76.01 THRU 01.76.02

77 ENGINE INDICATING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.01 THRU 01.77.06

78 EXHAUST. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.01 THRU 01.78.06

79 OIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.01 THRU 01.79.04

80 STARTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.01 THRU 01.80.02

CONFIGURATION DEVIATION LIST - SECTION 02

- - CDL TABLE OF CONTENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.00.01 THRU 02.00.04

- - CDL INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.01.01 THRU 02.01.02

21 AIR CONDITIONING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.21.01 THRU 02.21.02

23 COMMUNICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.23.01 THRU 02.23.02

27 FLIGHT CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.01 THRU 02.27.20

28 FUEL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.01 THRU 02.28.0230 ICE AND RAIN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.30.01 THRU 02.30.02

32 LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.01 THRU 02.32.02

33 LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.01 THRU 02.33.10

49 AIRBORNE AUXILIARY POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.49.01 THRU 02.49.02

51 STRUCTURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.01 THRU 02.51.04

52 DOORS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.01 THRU 02.52.36

53 FUSELAGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.01 THRU 02.53.04

54 NACELLE/PAYLON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.01 THRU 02.54.08

57 WINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.01 THRU 02.57.04

71 STRUCTURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.01 THRU 02.71.02

78 EXHAUST. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.78.01 THRU 02.78.02

* * *

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SYSTEM PAGE REV NO. DATE

LOG OF REVISION 00.00.01 Rev 07 12 FEB 12

LOG OF REVISION 00.00.02 Rev 07 12 FEB 12

CONTENTS 00.01.01 Rev 10 30 JUN 12

CONTENTS 00.01.02 Rev 07 12 FEB 12

TABLE OF CONTENTS 00.02.01 Rev 10 30 JUN 12

TABLE OF CONTENTS 00.02.02 Rev 07 12 FEB 12

LIST OF EFFECTIVE PAGES 00.03.01 Rev 10 30 JUN 12


LIST OF EFFECTIVE PAGES 00.03.03 Rev 09 01 MAY 12

LIST OF EFFECTIVE PAGES 00.03.04 Rev 07 12 FEB 12












LIST OF EFFECTIVE PAGES 00.03.16 Rev 10 30 JUN 12LIST OF EFFECTIVE PAGES 00.03.17 Rev 09 01 MAY 12






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MINIMUM EQUIPMENT LIST - SECTION 01


TABLE OF CONTENTS 01.00.02 Rev 09 01 MAY 12




















TABLE OF CONTENTS 01.00.22 Rev 07 12 FEB 12TABLE OF CONTENTS 01.00.23 Rev 10 30 JUN 12




MEL INTRODUCTION 01.01.01 Rev 07 12 FEB 12






GENERAL 01.02.01 Rev 07 12 FEB 12

GENERAL 01.02.02 Rev 07 12 FEB 12

00.03.02

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ECAM MESSAGES 01.03.01 Rev 07 12 FEB 12






















ECAM MESSAGES 01.03.23 Rev 07 12 FEB 12ECAM MESSAGES 01.03.24 Rev 09 01 MAY 12



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21 AIR CONDITIONING 01.21.01 Rev 07 12 FEB 12






















21 AIR CONDITIONING 01.21.23 Rev 07 12 FEB 1221 AIR CONDITIONING 01.21.24 Rev 07 12 FEB 12



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21 AIR CONDITIONING 01.21.37 Rev 10 30 JUN 1






21 AIR CONDITIONING 01.21.43 Rev 09 01 MAY 1






21 AIR CONDITIONING 01.21.49 Rev 09 01 MAY 121 AIR CONDITIONING 01.21.50 Rev 09 01 MAY 1



22 AUTO FLIGHT 01.22.01 Rev 07 12 FEB 1

22 AUTO FLIGHT 01.22.02 Rev 09 01 MAY 1













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23 COMMUNICATIONS 01.23.01 Rev 07 12 FEB 12




23 COMMUNICATIONS 01.23.05 Rev 09 01 MAY 12








23 COMMUNICATIONS 01.23.13 Rev 07 12 FEB 1223 COMMUNICATIONS 01.23.14 Rev 07 12 FEB 12











24 ELECTRICAL POWER 01.24.01 Rev 07 12 FEB 12






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24 ELECTRICAL POWER 01.24.08 Rev 10 30 JUN 1













25 EQUIPMENT & FURNISHNGS 01.25.01 Rev 07 12 FEB 1








25 EQUIPMENT & FURNISHNGS 01.25.09 Rev 07 12 FEB 125 EQUIPMENT & FURNISHNGS 01.25.10 Rev 07 12 FEB 1

25 EQUIPMENT & FURNISHNGS 01.25.11 Rev 09 01 MAY 1











25 EQUIPMENT & FURNISHNGS 01.25.22 Rev 10 30 JUN 1





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26 FIRE PROTECTION 01.26.01 Rev 07 12 FEB 12







26 FIRE PROTECTION 01.26.08 Rev 09 01 MAY 12













27 FLIGHT CONTROL 01.27.01 Rev 07 12 FEB 12


27 FLIGHT CONTROL 01.27.03 Rev 07 12 FEB 1227 FLIGHT CONTROL 01.27.04 Rev 07 12 FEB 12

















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27 FLIGHT CONTROL 01.27.23 Rev 10 30 JUN 1




















27 FLIGHT CONTROL 01.27.43 Rev 10 30 JUN 127 FLIGHT CONTROL 01.27.44 Rev 10 30 JUN 1















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28 FUEL 01.28.01 Rev 07 12 FEB 12

28 FUEL 01.28.02 Rev 07 12 FEB 12

28 FUEL 01.28.03 Rev 07 12 FEB 12

28 FUEL 01.28.04 Rev 07 12 FEB 12

28 FUEL 01.28.05 Rev 07 12 FEB 12

28 FUEL 01.28.06 Rev 07 12 FEB 12

28 FUEL 01.28.07 Rev 07 12 FEB 12

28 FUEL 01.28.08 Rev 07 12 FEB 12

28 FUEL 01.28.09 Rev 07 12 FEB 12

28 FUEL 01.28.10 Rev 07 12 FEB 12

28 FUEL 01.28.11 Rev 07 12 FEB 12

28 FUEL 01.28.12 Rev 07 12 FEB 12

28 FUEL 01.28.13 Rev 07 12 FEB 12

28 FUEL 01.28.14 Rev 07 12 FEB 12

28 FUEL 01.28.15 Rev 07 12 FEB 12

28 FUEL 01.28.16 Rev 07 12 FEB 12

28 FUEL 01.28.17 Rev 07 12 FEB 1228 FUEL 01.28.18 Rev 07 12 FEB 12

28 FUEL 01.28.19 Rev 07 12 FEB 12

28 FUEL 01.28.20 Rev 07 12 FEB 12

28 FUEL 01.28.21 Rev 07l 12 FEB 12

28 FUEL 01.28.22 Rev 07l 12 FEB 12

28 FUEL 01.28.23 Rev 07l 12 FEB 12

28 FUEL 01.28.24 Rev 07 12 FEB 12

28 FUEL 01.28.25 Rev 07 12 FEB 12

28 FUEL 01.28.26 Rev 07 12 FEB 12

28 FUEL 01.28.27 Rev 07 12 FEB 12

28 FUEL 01.28.28 Rev 07 12 FEB 12

28 FUEL 01.28.29 Rev 07 12 FEB 12

28 FUEL 01.28.30 Rev 07 12 FEB 12

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28 FUEL 01.28.31 Rev 07 12 FEB 1

28 FUEL 01.28.32 Rev 07 12 FEB 1

28 FUEL 01.28.33 Rev 07 12 FEB 1

28 FUEL 01.28.34 Rev 07 12 FEB 1

28 FUEL 01.28.35 Rev 07 12 FEB 1

28 FUEL 01.28.36 Rev 07 12 FEB 1

28 FUEL 01.28.37 Rev 07 12 FEB 1

28 FUEL 01.28.38 Rev 07 12 FEB 1

28 FUEL 01.28.39 Rev 07 12 FEB 1

28 FUEL 01.28.40 Rev 07 12 FEB 1

28 FUEL 01.28.41 Rev 07 12 FEB 1

28 FUEL 01.28.42 Rev 07 12 FEB 1

28 FUEL 01.28.43 Rev 07 12 FEB 1

28 FUEL 01.28.44 Rev 07 12 FEB 1

28 FUEL 01.28.45 Rev 07 12 FEB 1

28 FUEL 01.28.46 Rev 07 12 FEB 1

28 FUEL 01.28.47 Rev 07 12 FEB 1

28 FUEL 01.28.48 Rev 07 12 FEB 1

28 FUEL 01.28.49 Rev 07 12 FEB 1

28 FUEL 01.28.50 Rev 07 12 FEB 1

28 FUEL 01.28.51 Rev 07 12 FEB 1

28 FUEL 01.28.52 Rev 07 12 FEB 1

28 FUEL 01.28.53 Rev 07 12 FEB 128 FUEL 01.28.54 Rev 07 12 FEB 1

28 FUEL 01.28.55 Rev 07 12 FEB 1

28 FUEL 01.28.56 Rev 07 12 FEB 1

28 FUEL 01.28.57 Rev 07 12 FEB 1

28 FUEL 01.28.58 Rev 07 12 FEB 1

28 FUEL 01.28.59 Rev 07 12 FEB 1

28 FUEL 01.28.60 Rev 07 12 FEB 1

28 FUEL 01.28.61 Rev 07 12 FEB 1

28 FUEL 01.28.62 Rev 07 12 FEB 1

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29 HYDRAULIC 01.29.01 Rev 07 12 FEB 12




















30 ICE AND RAIN PROTECTION 01.30.01 Rev 07 12 FEB 12


30 ICE AND RAIN PROTECTION 01.30.03 Rev 07 12 FEB 1230 ICE AND RAIN PROTECTION 01.30.04 Rev 07 12 FEB 12





30 ICE AND RAIN PROTECTION 01.30.09 Rev 10 30 JUN 12






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31 INDICATING/RECORDING SYSTEM 01.31.01 Rev 07 12 FEB 1










31 INDICATING/RECORDING SYSTEM 01.31.11 Rev 07 12 FEB 131 INDICATING/RECORDING SYSTEM 01.31.12 Rev 07 12 FEB 1







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32 LANDING GEAR 01.32.01 Rev 07 12 FEB 12














32 LANDING GEAR 01.32.15 Rev 07 12 FEB 1232 LANDING GEAR 01.32.16 Rev 07 12 FEB 12




32 LANDING GEAR 01.32.20 Rev 10 30 JUN 12

32 LANDING GEAR 01.32.21 Rev 09 01 MAY 12










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32 LANDING GEAR 01.32.40 Rev10 30 JUN 1



















33 LIGHTS 01.33.01 Rev07 12 FEB 1233 LIGHTS 01.33.02 Rev07 12 FEB 12

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33 LIGHTS 01.33.03 Rev 10 30 JUN 12

33 LIGHTS 01.33.04 Rev 07 12 FEB 12

33 LIGHTS 01.33.05 Rev 07 12 FEB 12

33 LIGHTS 01.33.06 Rev 07 12 FEB 12

33 LIGHTS 01.33.07 Rev 10 30 JUN 12

33 LIGHTS 01.33.08 Rev 07 12 FEB 12

33 LIGHTS 01.33.09 Rev 07 12 FEB 12

33 LIGHTS 01.33.10 Rev 07 12 FEB 12

33 LIGHTS 01.33.11 Rev 07 12 FEB 12

33 LIGHTS 01.33.12 Rev 07 12 FEB 12

34 NAVIGATION 01.34.01 Rev 07 12 FEB 12












34 NAVIGATION 01.34.13 Rev 09 01 MAY 1234 NAVIGATION 01.34.14 Rev 07 12 FEB 12












34 NAVIGATION 01.34.26 Rev 10 30 JUN 12






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35 OXYGEN 01.35.01 Rev 07 12 FEB 1

35 OXYGEN 01.35.02 Rev 07 12 FEB 1

35 OXYGEN 01.35.03 Rev 07 12 FEB 1

35 OXYGEN 01.35.04 Rev 07 12 FEB 1

35 OXYGEN 01.35.05 Rev 07 12 FEB 1

35 OXYGEN 01.35.06 Rev 07 12 FEB 1

35 OXYGEN 01.35.07 Rev 07 12 FEB 1

35 OXYGEN 01.35.08 Rev 07 12 FEB 1

36 PNEUMATIC 01.36.01 Rev 07 12 FEB 1


36 PNEUMATIC 01.36.03 Rev 09 01 MAY 12










38 WATER/WASTE 01.38.01 Rev 07 12 FEB 12

38 WATER/WASTE 01.38.02 Rev 09 01 MAY 12

46 INFORMATION SYSTEM 01.46.01 Rev 07 12 FEB 1246 INFORMATION SYSTEM 01.46.02 Rev 07 12 FEB 1

47 INERT GAS SYSTEM 01.47.01 Rev 07 12 FEB 1

47 INERT GAS SYSTEM 01.47.02 Rev 07 12 FEB 1

49 AIRBORNE AUXILIARYPOWER 01.49.01 Rev 07 12 FEB 1

49 AIRBORNE AUXILIARYPOWER 01.49.02 Rev 07 12 FEB 1

52 DOORS 01.52.01 Rev 07 12 FEB 1

52 DOORS 01.52.02 Rev 07 12 FEB 1

52 DOORS 01.52.03 Rev 07 12 FEB 1

52 DOORS 01.52.04 Rev 07 12 FEB 1

52 DOORS 01.52.05 Rev 07 12 FEB 1

52 DOORS 01.52.06 Rev 07 12 FEB 1

52 DOORS 01.52.07 Rev 07 12 FEB 1

52 DOORS 01.52.08 Rev 07 12 FEB 1

52 DOORS 01.52.09 Rev 07 12 FEB 1

52 DOORS 01.52.10 Rev 07 12 FEB 1

01 MAY 12

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52 DOORS 01.52.11 Rev 07 12 FEB 12

52 DOORS 01.52.12 Rev 07 12 FEB 12

52 DOORS 01.52.13 Rev 07 12 FEB 12

52 DOORS 01.52.14 Rev 07 12 FEB 12

52 DOORS 01.52.15 Rev 07 12 FEB 12

52 DOORS 01.52.16 Rev 07 12 FEB 12

52 DOORS 01.52.17 Rev 07 12 FEB 12

52 DOORS 01.52.18 Rev 07 12 FEB 12

52 DOORS 01.52.19 Rev 07 12 FEB 12

52 DOORS 01.52.20 Rev 07 12 FEB 12

52 DOORS 01.52.21 Rev 07 12 FEB 12

52 DOORS 01.52.22 Rev 07 12 FEB 12

52 DOORS 01.52.23 Rev 07 12 FEB 12

52 DOORS 01.52.24 Rev 07 12 FEB 12

52 DOORS 01.52.25 Rev 07 12 FEB 12

52 DOORS 01.52.26 Rev 07 12 FEB 12

52 DOORS 01.52.27 Rev 07 12 FEB 12

52 DOORS 01.52.28 Rev 07 12 FEB 12

52 DOORS 01.52.29 Rev 07 12 FEB 12

52 DOORS 01.52.30 Rev 07 12 FEB 12

52 DOORS 01.52.31 Rev 07 12 FEB 12

52 DOORS 01.52.32 Rev 07 12 FEB 12

52 DOORS 01.52.33 Rev 07 12 FEB 1252 DOORS 01.52.34 Rev 07 12 FEB 12

52 DOORS 01.52.35 Rev 07 12 FEB 12

52 DOORS 01.52.36 Rev 07 12 FEB 12

52 DOORS 01.52.37 Rev 09 01 MAY 12

52 DOORS 01.52.38 Rev 07 12 FEB 12

56 WINDOWS 01.56.01 Rev 07 12 FEB 12

56 WINDOWS 01.56.02 Rev 07 12 FEB 12

56 WINDOWS 01.56.03 Rev 07 12 FEB 12

56 WINDOWS 01.56.04 Rev 07 12 FEB 12

70 ENGINES 01.70.01 Rev 07 12 FEB 12

70 ENGINES 01.70.02 Rev 07 12 FEB 12

73 ENGINE FUEL AND CONTROL 01.73.01 Rev 07 12 FEB 12

73 ENGINE FUEL AND CONTROL 01.73.02 Rev 07 12 FEB 12

73 ENGINE FUEL AND CONTROL 01.73.03 Rev 10 30 JUN 12

73 ENGINE FUEL AND CONTROL 01.73.04 Rev 10 30 JUN 12

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74 IGNITION 01.74.01 Rev 07 12 FEB 1

74 IGNITION 01.74.02 Rev 07 12 FEB 1

74 IGNITION 01.74.03 Rev 07 12 FEB 1

74 IGNITION 01.74.04 Rev 07 12 FEB 1

76 ENGINE CONTROLS 01.76.01 Rev 07 12 FEB 1

76 ENGINE CONTROLS 01.76.02 Rev 07 12 FEB 1

77 ENGINE INDICATING 01.77.01 Rev 07 12 FEB 1






78 EXHAUST 01.78.01 Rev 07 12 FEB 1

78 EXHAUST 01.78.02 Rev 07 12 FEB 1

78 EXHAUST 01.78.03 Rev 07 12 FEB 1

78 EXHAUST 01.78.04 Rev 07 12 FEB 1

78 EXHAUST 01.78.05 Rev 07 12 FEB 1

78 EXHAUST 01.78.06 Rev 07 12 FEB 1

79 OIL 01.79.01 Rev 07 12 FEB 1

79 OIL 01.79.02 Rev 07 12 FEB 1

79 OIL 01.79.03 Rev 07 12 FEB 1

79 OIL 01.79.04 Rev 07 12 FEB 1

80 STARTING 01.80.01 Rev 07 12 FEB 180 STARTING 01.80.02 Rev 07 12 FEB 1

12 FEB 12

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CONFIGURATION DEVIATION LIST - SECTION 02





CDL INTRODUCTION 02.01.01 Rev 07 12 FEB 12

CDL INTRODUCTION 02.01.02 Rev 07 12 FEB 12





27 FLIGHT CONTROLS 02.27.01 Rev 07 12 FEB 12











27 FLIGHT CONTROLS 02.27.12 Rev 07 12 FEB 1227 FLIGHT CONTROLS 02.27.13 Rev 07 12 FEB 12








28 FUEL 02.28.01 Rev 07 12 FEB 12

28 FUEL 02.28.02 Rev 07 12 FEB 12





00.03.20



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33 LIGHTS 02.33.01 Rev 07 12 FEB 1

33 LIGHTS 02.33.02 Rev 07 12 FEB 1

33 LIGHTS 02.33.03 Rev 07 12 FEB 1

33 LIGHTS 02.33.04 Rev 07 12 FEB 1

33 LIGHTS 02.33.05 Rev 07 12 FEB 1

33 LIGHTS 02.33.06 Rev 07 12 FEB 1

33 LIGHTS 02.33.07 Rev 07 12 FEB 1

33 LIGHTS 02.33.08 Rev 07 12 FEB 1

33 LIGHTS 02.33.09 Rev 07 12 FEB 1

33 LIGHTS 02.33.10 Rev 07 12 FEB 1

49 APU 02.49.01 Rev 07 12 FEB 1

49 APU 02.49.02 Rev 07 12 FEB 1

51 STRUCTURE 02.51.01 Rev 07 12 FEB 1




52 DOORS 02.52.01 Rev 07 12 FEB 1

52 DOORS 02.52.02 Rev 07 12 FEB 1

52 DOORS 02.52.03 Rev 07 12 FEB 1

52 DOORS 02.52.04 Rev 07 12 FEB 1

52 DOORS 02.52.05 Rev 07 12 FEB 1

52 DOORS 02.52.06 Rev 07 12 FEB 1

52 DOORS 02.52.07 Rev 07 12 FEB 152 DOORS 02.52.08 Rev 07 12 FEB 1

52 DOORS 02.52.09 Rev 07 12 FEB 1

52 DOORS 02.52.10 Rev 07 12 FEB 1

52 DOORS 02.52.11 Rev 07 12 FEB 1

52 DOORS 02.52.12 Rev 07 12 FEB 1

52 DOORS 02.52.13 Rev 07 12 FEB 1

52 DOORS 02.52.14 Rev 07 12 FEB 1

52 DOORS 02.52.15 Rev 07 12 FEB 1

52 DOORS 02.52.16 Rev 07 12 FEB 1

52 DOORS 02.52.17 Rev 07 12 FEB 1

52 DOORS 02.52.18 Rev 07 12 FEB 1

52 DOORS 02.52.19 Rev 07 12 FEB 1

52 DOORS 02.52.20 Rev 07 12 FEB 1

52 DOORS 02.52.21 Rev 07 12 FEB 1

52 DOORS 02.52.22 Rev 07 12 FEB 1

52 DOORS 02.52.23 Rev 07 12 FEB 1

52 DOORS 02.52.24 Rev 07 12 FEB 1

12 FEB 12

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52 DOORS 02.52.25 Rev 07 12 FEB 12

52 DOORS 02.52.26 Rev 07 12 FEB 12

52 DOORS 02.52.27 Rev 07 12 FEB 12

52 DOORS 02.52.28 Rev 07 12 FEB 12

52 DOORS 02.52.29 Rev 07 12 FEB 12

52 DOORS 02.52.30 Rev 07 12 FEB 12

52 DOORS 02.52.31 Rev 07 12 FEB 12

52 DOORS 02.52.32 Rev 07 12 FEB 12

52 DOORS 02.52.33 Rev 07 12 FEB 12

52 DOORS 02.52.34 Rev 07 12 FEB 12

52 DOORS 02.52.35 Rev 07 12 FEB 12

52 DOORS 02.52.36 Rev 07 12 FEB 12

52 DOORS 02.52.37 Rev 07 12 FEB 12

52 DOORS 02.52.38 Rev 07 12 FEB 12

53 FUSELAG 02.53.01 Rev 07 12 FEB 12

53 FUSELAG 02.53.02 Rev 07 12 FEB 12

53 FUSELAG 02.53.03 Rev 07 12 FEB 12

53 FUSELAG 02.53.04 Rev 07 12 FEB 12

54 NACELLES / PYL 02.54.01 Rev 07 12 FEB 12




54 NACELLES / PYL 02.54.05 Rev 07 12 FEB 1254 NACELLES / PYL 02.54.06 Rev 07 12 FEB 12







71 POWER PLANT 02.71.01 Rev 07 12 FEB 12

71 POWER PLANT 02.71.02 Rev 07 12 FEB 12

78 EXHAUST 02.78.01 Rev 07 12 FEB 12

78 EXHAUST 02.78.02 Rev 07 12 FEB 12

* * *

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ITEM PAG

MEL TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.00.0

FAA MMEL Preamble . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.0

Definitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.0ECAM General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.02.0

ECAM Messages Cross Reference List. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.03.0

ATA 21 - AIR CONDITIONING

21-00-03 AFT CRG HEAT MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-00-04 TEMP CTL 1(2) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-01-01 AIR COND Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-01-02 CABIN PRESS Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-01-03 CARGO VENT Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-01-04 VENTILATION Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-07-01 Indications on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-07-02 Indications on the CAB PRESS SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-07-03 Indications on the COND SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-07-04 Indications on the CRUISE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-09-01 VENT BLOWER FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-09-02 VENT EXTRACT FAULT Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-09-03 CAB PR SAFETY VALVE OPEN Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-21-01 Cabin Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-23-01 Lavatory and Galley Extraction Fan. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.0

21-26-01 Avionics Blower Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.1

21-26-02 Avionics Extract Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.1

21-26-03 Avionics Skin Exchanger Inlet Bypass Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2

21-26-04 Avionics Skin Air Outlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2

21-26-05 Avionics Skin Air Inlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2

21-26-06 Avionics Skin Exchanger Isolation Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2

21-26-07 Avionics Skin Exchanger Outlet Bypass Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2

21-26-08 Avionics Air Conditioning Inlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.2

21-26-09 Avionics Ventilation Filte . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.3

21-26-10 Avionics Equipment Ventilation Computer (AEVC) . . . . . . . . . . . . . . . . . . . . . . . . 01.21.3

21-28-03 AFT Cargo Extraction Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.3

21-28-04 AFT Cargo Isolation Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.3

21-31-01 Automatic Cabin Pressure Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .(CPC, Outflow Valve AUTO Channel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.37

21-31-02 Manual Cabin Pressure Control System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

(MAN V/S CTL selector, Outflow Valve MAN Channel). . . . . . . . . . . . . . . . . . . . . 01.21.3

21-31-03 Pressure Safety Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.4

21-31-04 Landing Elevation Selection AUTO Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.4

30 JUN 12MEL

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ITEM PAGE

ATA 21 - AIR CONDITIONING (Cont’d)

21-31-05 Landing Elevation Selection MAN Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.41

21-43-02 AFT Cargo Compartment Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.41

21-51-02 Pack Flow Selection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.43

21-51-03 Pack Flow Sensor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.43

21-52-01 Air Conditioning Pack. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.46

21-52-02 Air Conditioning Pack Ram Air Inlet Flap. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.47

21-55-01 Emergency Ram Air Inlet. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.48

21-61-01 Pack Turbine Bypass Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.49

21-63-02 Cockpit and Cabin Trim Air Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.49

21-63-03 Hot Air Pressure Regulating Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.50

21-63-04 Air Conditioning System Controller Channel (COND CTL 1(2)-A(B)) . . . . . . . . . . 01.21.52

ATA 22 - AUTO FLIGHT

22-01-01 FAC pb-sw FAULT light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01

22-01-02 FAC pb-sw OFF light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01

22-05-01 AP Related Indications on the FMA. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01

22-05-02 A/THR Related Indications on the FMA. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01

22-05-03 Approach and Landing Capabilities on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02

22-05-04 Special Messages on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02

22-10-01 Autopilot (AP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02

22-10-02 Flight Director (FD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.0322-10-03 Take-over pb Priority Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.03

22-10-04 Take-over pb AP Disconnection Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.04

22-10-05 AUTO LAND lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.05

22-10-06 AP Disengagement Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.05

22-10-07 Sticks and Rudder Pedals Locking Solenoid in AP Mode . . . . . . . . . . . . . . . . . . . 01.22.05

22-30-01 Autothrust (A/THR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.06

22-30-02 Autothrust Instinctive Disconnect pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.06

22-30-03 Autothrust Disengagement Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.09

22-60-01 FAC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.10

22-60-02 FAC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.11

22-60-03 Windshear Detection System Predictive . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.12

22-60-04 Yaw Damper System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.13

22-70-01 Flight Management System (FMS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.13

22-70-02 Navigation Database . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.14

22-70-03 Performance Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.15

22-70-04 Fuel/Time Prediction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.15

01.00.02TABLE OF CONTENTS

A320/321MEL/CDL

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ITEM PAG

ATA 22 - AUTO FLIGHT( cont’d)

22-81-01 Auto Flight Control Panel (FCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.1

22-81-02 EFIS Control Panel (FCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.1

22-81-03 FCU Channel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.2

22-82-01 MCDU 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.2

22-82-02 MCDU 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.2

22-82-04 MCDU Annunciator light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.2

22-83-01 Flight Management and Guidance Computer (FMGC) . . . . . . . . . . . . . . . . . . . . . 01.22.2

ATA 23 - COMMUNICATIONS

23-00-01 CIDS 1(2) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.023-01-01 RCDR Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-01-02 CALLS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-09-01 COM HF 1(2) EMITTING Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-09-02 COM VHF 1(2)(3) EMITTING Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-10-01 HF System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-10-02 VHF System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-10-03 SATCOM Voice Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-13-01 Radio Management Panel (RMP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-13-02 RMP Selection Key . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-20-01 Aircraft Communications Addressing Reporting System (ACARS) . . . . . . . . . . . 01.23.0

23-20-02 SATCOM Data Mode. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.023-31-01 Passenger Address System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-40-01 Mechanical Call Horn. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-40-02 Flight Crew Interphone System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-40-03 Flight Crew to Ground Communication System. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-40-04 Service Interphone Jack . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-51-01 SELCAL Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-51-02 Boomset. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-51-03 Hand Microphone. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-51-04 Cockpit Loudspeaker. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-51-05 Cockpit Loudspeaker Volume Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.0

23-51-06 Sidestick Radio selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.1

23-52-01 CAPT and F/O ACP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.1

23-52-02 ACP 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.1

01 MAY 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 23 - COMMUNICATIONS ( cont’d)

23-52-03 Fourth Occupant ACP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11

23-52-04 ACP in the Avionics Compartment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11

23-52-05 ACP Transmission Key . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11

23-52-06 ACP Reception knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11

23-52-07 ACP Reception knob light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11

23-53-01 AUDIO SWITCHING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12

23-71-01 Cockpit Voice Recorder (CVR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12

23-72-01 Cockpit Door Surveillance System (CDSS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12

23-73-01 Cabin Intercommunication Data System (CIDS) . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.14

23-73-02 DEU A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.15

23-73-03 DEU B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.16

23-73-04 Cabin Individual Call . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.18

23-73-05 Cabin Loudspeaker . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.18

23-73-06 Handset . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.19

23-73-07 Prerecorded Announcement and Music Reproducer (PRAM) . . . . . . . . . . . . . . . 01.23.20

23-73-08 Cabin Assignment Module (CAM) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.21

23-73-10 Smoke Detection Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.21

23-74-01 FAP Display Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23

23-74-02 EMER pb on Hardkey FAP Sub-panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23

23-74-03 Other Controls on Hardkey FAP Sub-panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23

23-74-06 Door Bottle Pressure Monitoring on the FAP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23

23-74-08 Slide Pressure Monitoring on the FAP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24

23-74-09 Area Call Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24

23-74-10 Attendant Information Panel (AIP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24

23-74-11 Additional Attendant Panel (AAP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24


A320/321MEL/CDL

12 FEB 12MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 24 - ELECTRICAL POWER

24-00-01 DC BUS TIE MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-00-03 AC GEN MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-01-01 ELEC Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-01-02 EMER ELEC PWR Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-07-01 AC Generation Indications on the ELEC SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-07-02 DC Generation Indications on the ELEC SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-07-03 AC ESS BUS SHED Indication on the ELEC SD page . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-09-01 ELEC AC ESS BUS SHED Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-09-02 C/B TRIPPED Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-22-01 AC Main Generation (IDG, GCU, Line Contactor) . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.0

24-22-02 AC Bus Tie Control Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-23-01 AC Auxiliary Generation (APU Generator, GCU, Line Contactor) . . . . . . . . . . . . . 01.24.1

24-24-01 Emergency Generator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-24-02 RAT Extension Automatic Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-24-03 RAT Extension Manual Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-25-01 Manual Transfer to the AC BUS 2 (ALTN Function) . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-25-02 Automatic Transfer to the AC BUS 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-26-01 GALY & CAB Automatic Load Shed System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-26-02 GALY & CAB Manual Load Shed System (GALY & CAB pb-sw) . . . . . . . . . . . . . 01.24.1

24-26-03 Commercial Supply System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-28-01 Static Inverter AC Generation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-32-01 DC Main Generation (TR 1, TR 2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-34-01 DC Emergency Generation (ESS TR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-35-01 DC TIE Contactor 1PC1 (DC BUS 1-DC BAT BUS), . . . . . . . . . . . . . . . . . . . . . . . . . . . .

4PC (DC ESS BUSDC BAT BUS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-35-02 DC TIE Contactor 1PC2 (DC BUS 2-DC BAT BUS) . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-38-01 BAT 1(2) Channel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-38-02 Battery Charger Limiter (BCL) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-38-03 Battery Voltmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.1

24-41-01 Ground Power Control Unit (GPCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.2

24-41-02 External Power Receptacle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.2

30 JUN 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 25 - EQUIPMENT / FURNISHINGS

25-07-01 Passenger Door Slide Permanently Indicated Armed (A320) . . . . . . . . . . . . . . . . 01.25.01

25-07-01 Cabin Passenger Door / Emergency Exit Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Permanently Indicated Armed (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.01

25-07-02 Passenger Door Slide Permanently Indicated Not Armed (A320) . . . . . . . . . . . . . 01.25.02

25-07-02 Cabin Passenger Door / Emergency Exit Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Permanently Indicated Not Armed (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.02

25-07-03 Emergency Exit Slide Permanently Indicated Armed . . . . . . . . . . . . . . . . . . . . . . 01.25.03

25-07-04 Emergency Exit Slide Permanently Indicated Not Armed . . . . . . . . . . . . . . . . . . . 01.25.03

25-11-01 Pilot Seat Manual Horizontal Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04

25-11-02 Pilot Seat Manual Vertical Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04

25-11-03 Pilot Seat Recline Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04

25-11-04 Pilot Seat Other Manual Adjustments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04

25-11-05 Pilot Seat Electrical Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.05

25-11-06 Pilot Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.05

25-11-07 Pilot Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06

25-11-08 Pilot Sidestick Armrest Height Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06

25-11-09 Pilot Sidestick Armrest Pitch Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06

25-11-10 Pilot Sidestick Armrest Memory Position Display . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06

25-11-11 Pilot Inboard Armrest Vertical Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07

25-11-12 Pilot Seat Headrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07

25-12-01 Third Occupant Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07

25-12-02 Third Occupant Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07

25-12-03 Third Occupant Seat Abdominal Belt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08

25-12-04 Third Occupant Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08

25-12-05 Fourth Occupant Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08

25-12-06 Fourth Occupant Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08

25-12-07 Fourth Occupant Seat Abdominal Belt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08

25-12-08 Fourth Occupant Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09

25-13-01 Pilot Sliding Table . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09

25-13-02 Pilot Retractable Footrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09

25-20-01 Passenger Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09

25-20-03 Cabin Attendant Seat. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.10

25-28-01 Overhead Storage Bin(s)/Cabin and Galley storage Compartment/ Closest. . . . . 01.25.12

25-35-01 Galley Waste Compartment Flapper Door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.12

25-40-01 Toilet Waste Compartment Flapper Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.13


A320/321MEL/CDL

12 FEB 12MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 25 - EQUIPMENT / FURNISHINGS ( cont’d)

25-40-02 Exterior Lavatory Ashtray. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-40-03 Interior Lavatory Ashtray . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-50-01 Cargo Loading System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-50-02 Decompression Panels in the Cargo Compartments. . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-50-03 Sidewall Linings and Ceiling Panels in the Cargo Compartments. . . . . . . . . . . . . 01.25.1

25-50-04 Cargo Compartment Restraint Components (Nets, Attach Points, Stanchions) . . 01.25.1

25-62-01 Cabin Passenger Door Slide or Slide Raft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-62-02 Overwing Emergency Exit Slide or Slide Raft (A320) . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-62-03 Emergency Exit Slide or Slide Raft (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-62-04 SLIDE ARMED light (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-62-04 SLIDE ARMED light (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-62-05 Survival Kit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-62-06 Passenger Door CHECK SLIDE PRESSURE Message on . . . . . . . . . . . . . . . . . . . . . . .

Flight Attendant Panel (FAP) (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.17

25-62-06 Passenger Door CHECK SLIDE PRESSURE Message on . . . . . . . . . . . . . . . . . . . . . . .

Flight Attendant Panel (FAP) (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.18

25-62-07 Overwing Emergency Exit CHECK SLIDE PRESSURE . . . . . . . . . . . . . . . . . . . . . . . . . .

Message on Flight Attendant Panel (FAP) (A320). . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-62-08 Overwing Escape Life Line . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.1

25-63-01 Emergency Evacuation Signaling System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

(COMMAND pbsw, HORN SHUT OFF pb, CAPT&PURS and CAPT sw). . . . . . . 01.25.1

25-64-01 First Aid Kit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-64-02 Emergency Medical Kit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.225-64-03 Automated External Defibrillator (AED) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-65-01 Cockpit Flashlight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-65-02 Cabin Flashlight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-65-03 Crash Axe/Crowbar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-65-04 Emergency Locator Transmitter (ELT). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-65-05 Fireproof Gloves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-65-06 Megaphone . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-66-01 Life Vest. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-66-02 Supplementary Life Raft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-70-01 Non-Essential Equipment & furnishings (NEF) . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

25-70-04 Movie/stereo Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.225-70-05 Overhead Reading Lamp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.2

30 JUN 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 26 - FIRE PROTECTION

26-00-01 SMOKE MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01

26-01-01 FIRE Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01

26-01-02 CARGO SMOKE Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05

26-12-01 Engine Fire Detection Loop A on the Engine 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05

26-12-02 Engine Fire Detection Loop A on the Engine 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05

26-12-03 Engine Fire Detection Loop B on the Engine 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06

26-12-04 Engine Fire Detection Loop B on the Engine 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06

26-12-05 FIRE light on the ENG MASTER Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06

26-13-01 APU Fire Detection Loop A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06

26-13-02 APU Fire Detection Loop B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.07

26-15-01 Avionics Smoke Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.07

26-16-01 Smoke Detector in the FWD Cargo Compartment (A320). . . . . . . . . . . . . . . . . . . 01.26.08

26-16-01 Smoke Detector in the FWD Cargo Compartment (A321). . . . . . . . . . . . . . . . . . . 01.26.09

26-16-02 Smoke Detector in the AFT and the BULK Cargo Compartments (A321). . . . . . . 01.26.10

26-16-02 Smoke Detector in the AFT and the BULK Cargo Compartments (A320). . . . . . . 01.26.11

26-17-01 Lavatory Smoke Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.12

26-22-01 APU Automatic Fire Extinguishing Control on Ground . . . . . . . . . . . . . . . . . . . . . 01.26.13

26-22-02 APU Fire Extinguisher Overpressure Indication (Red Disc) . . . . . . . . . . . . . . . . . 01.26.14

26-22-03 Squib of the APU Fire Extinguisher Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.15

26-22-04 APU Fire Extinguisher Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.15

26-22-05 APU AUTO EXTING TEST pb-sw on the Maintenance Panel. . . . . . . . . . . . . . . . 01.26.16

26-22-06 APU FIRE light on the External Power Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.16

26-22-07 APU SHUT OFF pb on the External Power Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.17

26-23-01 Cargo Agent Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.17

26-23-02 Squib of the Cargo Bottle 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.19

26-24-01 Portable Fire Extinguisher . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.19

26-25-01 Lavatory Waste Bin Fire Extinguishing System . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.20


A320/321MEL/CDL

01 MAY 12MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 27 - FLIGHT CONTROLS

27-00-01 F/CTL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-00-02 SFCS MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-01-01 FLT CTL Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-01 Aileron Actuator Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-02 Aileron Position Indication on the F/CTL SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-03 Elevator Actuator Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-04 Elevator Position Indication on the F/CTL SD page. . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-05 Pitch Trim Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-06 Rudder Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-07 Rudder Trim Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-08 Rudder Travel Limiter Position Indication on the F/CTL SD page . . . . . . . . . . . . . 01.27.0

27-07-09 ELAC Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-10 SEC Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.0

27-07-11 Spoilers/ Speed brakes Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . 01.27.1

27-07-12 Spoilers/ Speed brakes Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . 01.27.1

27-08-01 Flap Position Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-08-02 Slat Position Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-14-01 Left Aileron Blue Servo-Control (Controlled by ELAC 1) . . . . . . . . . . . . . . . . . . . . 01.27.1

27-14-02 Left Aileron Green Servo- Control (Controlled by ELAC 2) . . . . . . . . . . . . . . . . . . 01.27.1

27-14-03 Right Aileron Green Servo- Control (Controlled by ELAC 1) . . . . . . . . . . . . . . . . . 01.27.1

27-14-04 Right Aileron Blue Servo- Control (Controlled by ELAC 2) . . . . . . . . . . . . . . . . . . 01.27.1

27-21-01 Rudder Pedal Adjustment System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-22-01 Rudder Trim System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-22-02 Manual Rudder Trim Reset Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-22-03 Rudder Trim Position Indication on the Center Pedestal. . . . . . . . . . . . . . . . . . . . 01.27.1

27-23-01 Rudder Travel Limiter System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-34-01 Elevator Servo Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-34-02 Elevator Servo Control Position Transducer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-40-01 Stabilizer Mechanical Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-40-02 Stabilizer Actuator Electrical Motor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.1

27-51-01 SFCC Flap Channel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2

27-51-02 SFCC Slat Channel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2

27-51-03 Flap Wing Tip Brakes Solenoid . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.227-54-01 Flap Hydraulic Motor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2

27-54-02 Flap PCU Valve Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2

27-54-03 Flap Pressure Off Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2

27-64-01 Spoiler 5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2

27-64-02 Spoiler 1 or 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.2

30 JUN 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 27 - FLIGHT CONTROLS (Cont’d)

27-64-03 Spoiler 2 or 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.25

27-64-04 Spoilers 1 and 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.26

27-64-05 Spoilers 3 and 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.29

27-81-01 Slat Wing Tip Brakes Solenoids. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30

27-84-01 Slats Hydraulic Motor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30

27-84-02 Slat PCU Valve Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30

27-84-03 Slat Pressure- Off Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30

27-92-01 Speed brake Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.31

27-92-02 Ground Spoiler Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.34

27-92-03 SIDESTICK PRIORITY light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35

27-92-04 Sidestick Dual Input Visual Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35

27-92-05 Sidestick Dual Input Aural Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35

27-93-01 ELAC 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35

27-93-02 ELAC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.44

27-93-03 Pitch Normal Law. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.45

27-94-01 SEC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.45

27-94-02 SEC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.51

27-94-03 SEC 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.55

27-95-01 FCDC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.57

27-95-02 FCDC 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.57

ATA 28 - FUEL

28-00-01 FUEL MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01

28-01-01 FUEL Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01

28-07-01 Fuel Quantity Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.05

28-07-02 Fuel Temperature Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . 01.28.22

28-07-03 Tank Pump Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.23

28-07-04 Valve Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.23

28-09-01 FUEL L(R) INNER(OUTER) TK HI TEMP Alert (A320) . . . . . . . . . . . . . . . . . . . . . 01.28.27

28-09-01 FUEL L(R) WING TK HI TEMP Alert (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.28

28-09-02 FUEL L(R) INNER(OUTER) TK LO TEMP Alert (A320) . . . . . . . . . . . . . . . . . . . . 01.28.30

28-09-02 FUEL L(R) WING TK LO TEMP Alert (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.31

28-09-03 FUEL ACT XFR FAULT Alert (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.33

28-12-01 Overpressure Protector between Inner and Outer Tank (A320) . . . . . . . . . . . . . . 01.28.33

28-12-02 Overpressure Protector in Vent Surge Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36

28-12-03 Overpressure Protector in The Inner Tank (A320). . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36

28-12-03 Overpressure Protector in The Wing Tank (A321). . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36


A320/321MEL/CDL

30 JUN 12MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 28 - FUEL (Cont’d )

28-12-04 Overpressure Protector between Center and Inner Tank (A320) . . . . . . . . . . . . . 01.28.3

28-12-04 Overpressure Protector between Center and Wing Tank (A321) . . . . . . . . . . . . . 01.28.3

28-12-05 Overpressure Protector in the ACT (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . 01.28.3

28-15-01 LH Wing Transfer Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.3

28-15-02 RH Wing Transfer Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.3

28-20-01 Automatic Fuel Feed System (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-21-01 Wing Tank Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-21-02 Center Tank Pump (A320)(ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-21-02 Center Tank Pump (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-21-03 Wing Tank Pump Sequence Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-22-01 APU Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-23-01 Crossfeed Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-24-01 Engine LP Fuel Valve Electrical Motor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-25-01 Fuel Quantity Preselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-25-02 Fuel Quantity on the Refuel/Defuel Control Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-25-03 Refuel Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-25-04 Transfer Defuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-25-05 Exterior Refuel/Defuel Control Panel (A320 & A321) . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-26-01 Center Tank Transfer Valve (A321). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-28-01 ACT Auto Transfer System (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.4

28-28-02 ACT Transfer Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-28-03 ACT Transfer Pump. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-28-04 ACT Air Shutoff Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-28-05 ACT Inward Pressure Relief Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-28-06 ACT Vent Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-28-07 ACT Refuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-28-08 ACT Integrated Impact Wall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-28-09 ACT 1 Inlet Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-29-01 APU LP Fuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-43-01 Manual Magnetic Indicators (A320 & A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.5

28-46-01 High Level Detection System in the Inner Tank (A320). . . . . . . . . . . . . . . . . . . . . 01.28.6

28-46-01 High Level Detection System in the Wing Tank (A321). . . . . . . . . . . . . . . . . . . . . 01.28.6

28-46-02 High Level Detection System in the Center Tank (A320) . . . . . . . . . . . . . . . . . . . 01.28.628-46-02 High Level Detection System in the Center Tank (A320) (ACTs) . . . . . . . . . . . . . 01.28.6

28-46-03 High Level Detection System in the ACT (A320) (ACTs). . . . . . . . . . . . . . . . . . . . 01.28.6

28-46-04 Low Level Detection System in the Inner Tank (A320) . . . . . . . . . . . . . . . . . . . . . 01.28.6

28-46-04 Low Level Detection System in the Wing Tank (A321) . . . . . . . . . . . . . . . . . . . . . 01.28.6

28-46-05 Low Level Detection System in the ACT (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . 01.28.6

28-50-01 Fuel Quantity Indicating Computer (FQIC) Channel . . . . . . . . . . . . . . . . . . . . . . . 01.28.6

12 FEB 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 29 - HYDRAULIC POWER

29-01-01 HYD Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.01

29-01-02 Maintenance HYD Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.03

29-07-01 Yellow ELEC Pump Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . 01.29.03

29-07-02 Engine Driven Pump Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . 01.29.03

29-07-03 Fire Valve Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.03

29-07-04 PTU Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04

29-07-05 Reservoir Quantity Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . 01.29.04

29-07-06 RAT Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04

29-07-07 System Label Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04

29-07-08 System Pressure Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.29.06

29-09-01 HYD B(Y) ELEC PUMP LO PR Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08

29-09-02 HYD B(Y) ELEC PUMP OVHT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08

29-09-03 HYD G(Y) ENG 1(2) PUMP LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08

29-09-04 HYD G(B)(Y) RSVR LO AIR PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.10

29-09-05 HYD G(B)(Y) RSVR LO LVL Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.10

29-09-06 HYD G(B)(Y) RSVR OVHT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.11

29-09-07 HYD PTU FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.11

29-09-08 HYD RAT FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.12

29-09-09 HYD G(B)(Y)(B+G)(G+Y) (B+Y) SYS LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . 01.29.12

29-10-01 Engine Driven Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14

29-10-02 Engine Driven Pump Depressurization Function . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14

29-10-03 Blue System Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14

29-10-04 Hydraulic System Accumulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15

29-10-05 Yellow Brake Accumulator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15

29-10-07 Engine Pump Fire Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15

29-10-08 Hydraulic System Filter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15

29-10-09 Hydraulic Case Drain Filter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16

29-22-01 Ram Air Turbine. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16

29-23-01 Power Transfer Unit (PTU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16

29-24-01 Yellow System Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.18


A320/321MEL/CDL

12 FEB 12MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 30 - ICE AND RAIN PROTECTION

30-00-01 ICE DETECT MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0

30-01-01 ANTI ICE Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0

30-01-02 Wiper Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0

30-07-01 ANTI ICE Indication on the BLEED SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0

30-07-02 Arrow Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0

30-11-01 Wing Anti-Ice Control Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0

30-21-01 Engine Anti-Ice Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.0

30-31-01 Probe Heat Computer (PHC). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.1

30-31-02 Pitot Heater . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.1

30-31-03 Static Ports Heater. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.1

30-31-04 Angle of Attack (AOA) Probes Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.1

30-31-05 TAT Probes Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-42-01 Window Heat Computer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-42-02 Fixed Lateral Window and Sliding Window Heating . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-42-03 Windshield Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-42-04 PROBES/ WINDOW HEAT pb-sw AUTO Control . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-42-05 PROBES/WINDOW HEAT pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-45-01 Windshield Wiper. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-45-02 Windshield Wiper PARK Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-45-03 Rain Repellent System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-71-01 Waste Water Drain Mast Heating System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-71-02 Waste Water Drain Line Ice Protection System. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-81-01 Ice Detection System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-81-02 External Visual Icing Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

30-81-03 Lighting of External Visual Icing Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.2

ATA 31 - INDICATING / RECORDING SYSTEMS

31-00-01 QAR MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-00-02 ACMS MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-00-03 DAR MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-00-04 CFDIU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-00-05 DMC 1/3 MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-00-06 DMC 2/3 MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-05-01 AP Related Indications on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-05-02 A/THR Related Indications on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-05-03 Approach and Landing Capabilities on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-05-04 Special Messages on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

31-05-05 Actual Airspeed Reference Line and Scale Indications on the PFD . . . . . . . . . . . 01.31.0

31-05-06 Mach Number Indication on the PFD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.0

30 JUN 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 31 - INDICATING / RECORDING SYSTEMS (Cont’d )

31-05-07 VMO/MMO Characteristic Speed Indication on the PFD. . . . . . . . . . . . . . . . . . . . 01.31.03

31-05-08 Altitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.03

31-05-09 Vertical Speed Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.03

31-05-10 Other Air Data Related Indications on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04

31-05-11 Attitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04

31-05-12 Heading Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04

31-06-01 Ground Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04

31-06-02 True Air Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04

31-06-04 Heading Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05

31-06-05 Position (Aircraft Symbol) Indication on the ND. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05

31-06-06 Navigation Station Information on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05

31-06-07 Chrono Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05

31-07-01 Indications on the System Display pages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05

31-07-02 Permanent Data Indications on the SD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.06

31-08-01 Engine Parameter Indications on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.06

31-08-02 Fuel On Board (FOB) Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07

31-08-03 MEMO Messages on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07

31-08-04 Slats/Flaps Position Indications on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07

31-20-01 Electrical Clock Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07

31-30-01 Centralized Fault Display System (CFDS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.08

31-30-02 Digital AIDS Recorder (DAR). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.08

31-30-03 Digital Flight Data Recorder (DFDR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09

31-30-04 Data Management Unit (DMU) part of Flight Data Interface . . . . . . . . . . . . . . . . . . . . . . . .

and Management Unit (FDIMU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09

31-30-05 Flight Data Interface Unit (FDIU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09

31-30-06 Quick Access Recorder (QAR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10

31-30-07 Printer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10

31-38-01 DATA LOADING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10

31-38-02 Data Loading Routing Box (DLRB) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10

31-38-03 Multipurpose Disk Drive Unit (MDDU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11

31-53-01 Flight Warning Computer (FWC) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11

31-53-02 MASTER CAUT Cancel Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11

31-53-03 MASTER WARN Cancel Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11

31-53-04 MASTER CAUT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11

31-53-05 MASTER WARN light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.12

31-53-06 Altitude Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.12

31-55-01 System Data Acquisition Concentrator (SDAC). . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13

31-56-01 System Page Manual Call pb onthe ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13

31-56-02 ALL pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13


A320/321MEL/CDL

12 FEB 12MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 31 - INDICATING / RECORDING SYSTEMS (Cont’d )

31-56-03 CLR pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1

31-56-04 EMER CANC pb on the ECP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1

31-56-05 RCL pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1

31-56-06 STS pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1

31-56-07 T.O CONFIG pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1

31-62-01 DMC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1

31-62-02 DMC 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1

31-62-03 DMC 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.1

31-63-01 PFDU 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2

31-63-02 PFDU 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2

31-63-03 NDU 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2

31-63-04 NDU 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2

31-63-05 SDU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2

31-63-06 EWDU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2

31-68-01 AIR DATA SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . . . . . . 01.31.2

31-68-02 ATT HDG SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . . . . . . 01.31.2

31-68-03 ECAM/ND XFR SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . 01.31.2

31-68-04 EIS DMC SWITCHING selector on the Center Pedestal. . . . . . . . . . . . . . . . . . . . 01.31.2

31-68-05 PFD/ND XFR pb on the Lateral Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.2

ATA 32 - LANDING GEAR

32-07-01 Brakes Temperature Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . 01.32.0

32-07-02 L/G Position Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-03 L/G Doors Position Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-04 L/G CTL Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-05 UP LOCK Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-06 [Y] N/W STEERING Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-07 Tire Pressure Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-08 ANTI SKID, [1], [2] Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-09 AUTO BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-10 [G] NORM BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-11 Release Brake Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1

32-07-12 ACCU PRESS/ACCU ONLY Indication on the WHEEL SD page . . . . . . . . . . . . . 01.32.1

32-07-13 [Y] ALTN BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.32.1

30 JUN 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 32 - LANDING GEAR (Cont’d)

32-09-01 BRAKES-N/WS MINOR FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.19

32-09-02 WHEEL TYRE LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.21

32-11-01 Main Gear Torque Link Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.22

32-12-01 Ground Opening Cable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.22

32-31-01 Landing Gear Control and Interface Unit (LGCIU). . . . . . . . . . . . . . . . . . . . . . . . . 01.32.23

32-31-02 Landing Gear Retracting System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.26

32-32-01 LGCIU 1 Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.26

32-32-02 LGCIU 2 RH L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.27

32-32-03 LGCIU 2 LH L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.29

32-32-04 LGCIU 2 Nose L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . 01.32.32

32-32-05 LGCIU 2 RH L/G Down Lock Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.33

32-32-06 LGCIU 2 LH L/G Down Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.34

32-32-07 LGCIU 2 Nose L/G Down Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . 01.32.35

32-32-08 LGCIU 2 RH L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.36

32-32-09 LGCIU 2 LH L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.37

32-32-10 LGCIU 2 Nose L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.38

32-32-11 LGCIU 2 RH L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.39

32-32-12 LGCIU 2 LH L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.39

32-32-13 LGCIU 2 Nose L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . 01.32.40

32-32-14 LGCIU 2 RH L/G Doors Closed Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . 01.32.41

32-32-15 LGCIU 2 LH L/G Doors Closed Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . 01.32.42

32-32-16 LGCIU 2 Nose L/G Doors Closed Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.43

32-33-01 Landing Gear Gravity Extension System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.43

32-41-01 Nose Wheel Tie Bolt . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.43

32-41-02 Main Wheel Tie Bolt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.44

32-42-01 Main Wheel Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.45

32-42-02 Green System Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.48

32-42-03 Braking/Steering Control Unit (BSCU) System 1. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.49

32-42-04 Braking/Steering Control Unit (BSCU) System 2. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.49

32-42-05 AUTO/BRK Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50

32-42-06 Tachometer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50

32-42-08 AUTO/BRK (LO,MED, MAX) pb-sw DECEL light . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50

32-42-09 AUTO/BRK (LO, MED, MAX) pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5132-44-01 Yellow System Brake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.51

32-44-02 ACCU PRESS Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.52

32-44-03 BRAKES Pressure Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.53



MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 32 - LANDING GEAR (Cont’d)

32-44-04 Alternate Braking Control Unit (ABCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-45-01 Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-47-01 Brake Temperature Monitoring Unit (BTMU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-48-01 Brake Fan System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-48-02 BRK FAN pb-sw HOT light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-48-03 BRK FAN pb-sw ON light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-51-01 Nose Wheel Steering Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-51-02 Rudder PEDALS DISC pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-51-03 NWS Electrical Deactivation Box. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-51-04 PARKING BRAKE light on the NWS Electrical Deactivation Box . . . . . . . . . . . . . 01.32.5

32-61-01 LDG GEAR Indicator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

32-61-02 DOWN Red Arrow light on the Landing Gear lever . . . . . . . . . . . . . . . . . . . . . . . . 01.32.5

ATA 33 - LIGHTS

33-01-01 ANN LT Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-01-02 SIGNS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-10-01 Cockpit General Illumination (Center & Main Instrument Lighting, . . . . . . . . . . . . . . . . . .

Console and Floor Lighting, Dome lights and Lighting Strips, Instrument . . . . . . . . . . . .

and Panel Integral Lighting, Map Holder Lighting, Center Pedestal Lighting) . . . . 01.33.0

33-20-01 Cabin General Illumination. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.033-20-02 Cabin Signs (No Smoking/Fasten Seat Belt/Return to Seat). . . . . . . . . . . . . . . . . 01.33.0

33-20-03 Lavatory Sign (Return to seat). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-30-01 Cargo and Service Compartment Lighting System . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-01 Navigation light System 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-02 Navigation light System 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-03 Landing light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-04 Landing light Extension/Retraction System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-05 Runway Turnoff lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-06 Taxi and Takeoff light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-07 Logo lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-08 Beacon light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.033-40-09 Wing Scan lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-40-10 Strobe light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-51-01 Exit Marking Sign (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-51-01 Exit Marking Sign (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-51-02 Exit Location Sign in the Main Aisle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.0

33-51-03 Overhead Emergency Lighting System in the Main Aisle . . . . . . . . . . . . . . . . . . . 01.33.0

30 JUN 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 33 - LIGHTS (Cont’d)

33-51-04 Overhead Emergency Lighting System in the Door Vicinity (A320). . . . . . . . . . . . 01.33.10

33-51-04 Overhead Emergency Lighting System in the Door Vicinity (A321). . . . . . . . . . . . 01.33.10

33-51-05 Floor Proximity Emergency Escape Path Marking System in the Main Aisle . . . . 01.33.10

33-51-07 Floor Proximity Emergency Escape Path Marking System Exit Marker . . . . . . . . 01.33.11

33-51-08 Overwing Emergency light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11

33-51-09 Overwing Exit Handle light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11

33-51-10 Escape Slide Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11

33-51-11 Lavatory Auxiliary light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11

ATA 34 - NAVIGATION

34-00-01 ADR (1)(2)(3) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01

34-00-02 IR MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01

34-01-01 ADIRS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01

34-01-02 GPWS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.04

34-05-01 Actual Airspeed Reference Line and Scale Indication on the PFD . . . . . . . . . . . . 01.34.04

34-05-02 Mach Number Indication on the PFD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.04

34-05-03 VMO/MMO Characteristic Speed Indication on the PFD. . . . . . . . . . . . . . . . . . . . 01.34.05

34-05-04 Altitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.05

34-05-05 Baro Reference Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.05

34-05-06 Vertical Speed in Inertial Mode Indication on the PFD . . . . . . . . . . . . . . . . . . . . . 01.34.05

34-05-07 Other Air Data Related Indications on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.0634-05-08 Attitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.06

34-05-09 Heading Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.06

34-06-01 Ground Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07

34-06-02 True Air Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07

34-06-03 Wind Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07

34-06-04 Heading Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07

34-06-05 Position (Aircraft Symbol) Indication on the ND. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07

34-06-06 Radio Navaids Indications on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07

34-06-07 Chrono Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08

34-10-01 ADR 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08

34-10-02 ADR 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08

34-10-03 ADR 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.10

34-10-04 IR 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.11


A320/321MEL/CDL

12 FEB 12MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 34 - NAVIGATION (Cont’d)

34-10-05 IR 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1

34-10-07 IR 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1

34-11-01 Angle of Attack (AOA) Sensor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1

34-11-02 CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR1 . . . . . . 01.34.1

34-11-03 CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR3 . . . . . . 01.34.1

34-11-04 F/O Total Air Temperature (TAT) Sensor Element Connected to ADR2 . . . . . . . . 01.34.1

34-21-05 Standby ALT Metric Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1

34-22-01 Standby Compass Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1

34-22-02 Standby Compass Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.1

34-23-01 ISIS Baro-Altitude Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-23-02 ISIS Airspeed Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-23-03 ISIS Bugs Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-23-04 ISIS Horizon Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-23-05 ISIS ILS Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-23-06 ISIS Mach Number Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-30-04 Instrument Landing System (ILS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness . . . . . . . . . . . . . . . . . . .

and Warning System (TAWS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-40-02 Radio Altimeter Automatic Callout. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-40-03 Radio Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-40-04 Traffic Collision Avoidance System (TCAS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-40-05 Weather Radar System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-40-06 Predictive Windshear Detection Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-40-07 PULL UP-GPWS pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-50-01 ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.2

34-50-03 ADF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3

34-50-04 DME. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3

34-50-05 VOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3

34-50-06 MARKER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3

34-50-09 Global Positioning System (GPS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.3

30 JUN 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 35 - OXYGEN

35-01-01 OXYGEN Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.01

35-07-01 Crew OXY High Pressure Indication on the DOOR/OXY SD page . . . . . . . . . . . . 01.35.02

35-07-02 Crew Oxygen REGUL LO PR Indication on the DOOR/OXY SD page . . . . . . . . . 01.35.03

35-10-01 Crew Oxygen Mask . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.03

35-10-02 Crew Oxygen Mask Microphone . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.03

35-10-03 Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc). . . . . . . . . . . . . 01.35.03

35-20-01 Passenger Oxygen Unit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.04

35-20-02 Cabin Attendant Oxygen Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.05

35-20-04 Galley Oxygen Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.05

35-20-05 Manual Release Tool. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.06

35-30-01 Flight Crew Portable Device . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.06

35-30-02 Cabin Attendant Portable Device. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.07

ATA 36 - PNEUMATIC

36-00-01 AIR BLEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01

36-01-01 ENG BLEED pbsw FAULT light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01

36-01-02 ENG BLEED pbsw OFF light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01

36-01-03 APU BLEED pb-sw FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01

36-01-04 APU BLEED pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01

36-07-01 APU Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . 01.36.02

36-07-02 Engine Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . 01.36.0236-07-03 Engine Bleed HP Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . 01.36.02

36-07-04 Engine Bleed Precooler Inlet Pressure Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.02

36-07-05 Engine Bleed Precooler Outlet Temperature Indication . . . . . . . . . . . . . . . . . . . . . . . . . . .

on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.02

36-07-06 X Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.36.03

36-11-01 Engine Bleed Air Supply System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.03

36-11-02 Engine Bleed Valve (PRV). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.05

36-11-03 Engine Bleed Overpressure Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.05

36-11-04 Engine Bleed Fan Air Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.06

36-11-05 Engine Bleed Air Precooler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.06


A320/321MEL/CDL

01 MAY 12MEL

7/23/2019 A 320321 Mel Cdl


ITEM PAG

ATA 36 - PNEUMATIC (Cont’d)

36-11-06 Engine Bleed IP Check Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0

36-11-07 Engine Bleed HP Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0

36-11-08 Bleed Monitoring Computer (BMC) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0

36-12-01 APU Bleed Air Supply System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0

36-12-02 APU Bleed Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.0

36-12-03 APU Bleed Check Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1

36-12-04 Automatic Control of the X Bleed Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1

36-22-01 Pylon Leak Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1

36-22-02 Wing Leak Detection System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1

36-22-03 APU Leak Detection Loop . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.1

ATA 38 - WATER/WASTE

38-10-01 Potable Water Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.38.0

38-30-01 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories). . . . . . . . 01.38.0

ATA 46 - INFORMATION SYSTEMS

46-11-01 Electronic Flight Bag (EFB) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.0

46-21-01 Air Traffic Service Unit (ATSU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.0

46-21-02 Datalink Control and Display Unit (DCDU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.0

46-21-03 ATC MSG pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.0

ATA 47 - INERT GAS SYSTEMS

47-00-01 FUEL INERT MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.47.0

ATA 49 - AIRBORNE AUXILIARY POWER

49-00-01 APU MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0

49-01-01 APU MASTER SW pb-sw FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.049-01-02 APU MASTER SW pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0

49-01-03 APU START pb-sw AVAIL light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0

49-01-04 APU START pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0

49-07-01 Indications on the APU SD Page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0

49-10-01 Power Plant (APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0

49-10-02 APU Air Intake Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.0

01 MAY 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 52 - DOORS

52-01-01 CKPT DOOR CONT Normal Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.01

52-01-02 CKPT DOOR CONT BK UP Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.02

52-01-03 CKPT DOOR BK UP Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.05

52-07-01 Passenger Door Permanently Indicated Open on the DOOR/OXY . . . . . . . . . . . . . . . . . .

SD page (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.10

52-07-01 Passenger Door/Emergency Exit Permanently . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Indicated Open on the DOOR/OXY SD page(A321) . . . . . . . . . . . . . . . . . . . . . . . 01.52.14

52-07-02 Passenger Door Permanently Indicated . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Closed on the DOOR/OXY SD page (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.18

52-07-02 Passenger Door/Emergency Exit Permanently Indicated Closed . . . . . . . . . . . . . . . . . . . .

on the DOOR/OXY SD page (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.19

52-07-03 Overwing Emergency Exit Permanently Indicated Open on the . . . . . . . . . . . . . . . . . . . . .DOOR/OXY SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.20

52-07-04 Overwing Emergency Exit Permanently Indicated Closed on the . . . . . . . . . . . . . . . . . . . .

DOOR/OXY SD page (A320). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.23

52-07-05 Cargo Door Indication on the DOOR/OXY SD page . . . . . . . . . . . . . . . . . . . . . . . 01.52.24

52-07-06 Avionics Compartment Access Door Indication on the . . . . . . . . . . . . . . . . . . . . . . . . . . . .

DOOR/OXY SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.25

52-10-01 Cabin Passenger Door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27

52-10-02 Overwing Emergency Exit (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27

52-10-03 Passenger Exit Stop Fitting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27

52-10-04 Door Damper Function (A320 & A321)). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27

52-10-05 Door Emergency Opening Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28

52-10-06 CHECK DOOR PRESSURE Message on the . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Flight Attendant Panel (FAP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28

52-10-07 Passenger Door Stay Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28

52-10-08 CABIN PRESSURE light (on Doors) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29

52-30-01 Cargo Door (FWD, AFT and BULK) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29

52-30-02 Cargo Door Actuator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29

52-30-03 Cargo Door Electrical Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.30

52-30-04 Cargo Door Locking Hooks and Spools (Rollers) . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.30

52-30-05 Cargo Door Hand Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31

52-30-06 Cargo Door Drift Pin. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31

52-30-07 Cargo Doors Open/Locked Indicator light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31

52-33-01 Cargo Door Balance Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.32

52-51-01 CDLS Normal System (Normal Control Unit, Switch and Lights on the . . . . . . . . . . . . . . .

CKPT DOOR Panel,Buzzer, Keypad) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.32

52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on . . . . . . . . . . . . . . . . .

the CKPT DOOR BK UP Panel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.34


A320/321MEL/CDL

12 FEB 12MEL

7/23/2019 A 320321 Mel Cdl


TEM PAG

ATA 52 - DOORS (Cont’d)

52-51-03 CDLS Buzzer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3

52-51-04 CDLS Keypad . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3

52-51-05 CDLS Keypad Green and Red LEDs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3

52-51-06 CDLS Door Release Strike (Catch, Spring, Solenoid, Bolt). . . . . . . . . . . . . . . . . . 01.52.3

52-53-01 COCKPIT DOOR FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3

52-53-02 COCKPIT DOOR OPEN light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3

52-53-03 LOCK Function of the COCKPIT DOOR sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3

52-53-04 UNLOCK Function of the COCKPIT DOOR sw. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.3

ATA 56 - WINDOWS

56-10-01 Front Windshield Note: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.0

56-10-02 Lateral Fixed/Sliding Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.0

56-10-03 Sliding Window Opening/Closing Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.0

56-20-01 Cabin Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.0

ATA 70- ENGINE

70-00-01 ENG FADEC MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.0

70-00-02 ENG EIU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.0

70-00-03 ENG EVMU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.0

ATA 73- ENGINE FUEL AND CONTROL

73-07-01 F. USED Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0

73-07-02 Fuel Filter Clog Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . 01.73.0

73-08-01 F. F. (Fuel Flow) Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0

73-09-01 ENG 1(2) FUEL FILTER CLOG Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0

73-10-01 Fuel Return Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0

73-10-03 Fuel Metering Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0

73-20-01 Flex Takeoff Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0

73-20-05 Minimum Idle on Ground . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.0

30 JUN 12MEL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 74 - IGNITION

74-07-01 Selected Igniter Indication on the ENGINE SD page. . . . . . . . . . . . . . . . . . . . . . . 01.74.01

74-09-01 ENG 1(2) IGN A(B)(A+B) FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.03

74-31-01 Ignition System A. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.03

74-31-02 Ignition System B. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.04

ATA 76 - ENGINE CONTROL

76-11-01 Thrust lever Position Sensor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.76.01

ATA 77 - ENGINE INDICATING

77-07-01 Indications on the CRUISE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.01

77-07-02 Indications on the ENGINE SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.02

77-08-01 EGT Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05

77-08-03 F.F. (Fuel Flow) Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05

77-08-04 N1 Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05

77-08-05 N2 Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05

ATA 78 - ENGINE EXHAUST

78-08-01 REV Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.0178-30-01 Thrust Reverser. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.01

78-30-02 Thrust Reverser Inhibition Relay sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.05

78-30-03 Thrust Reverser Shutoff Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.05

ATA 79 - ENGINE OIL

79-07-01 CLOG Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.01

79-07-02 Oil Pressure Indication and Advisory on the ENGINE SD page . . . . . . . . . . . . . . 01.79.01

79-07-03 Oil Quantity Indication on the ENGINE SD page. . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.02

79-07-04 Oil Temperature Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . 01.79.0279-09-01 ENG 1(2) OIL LO PR Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.02

79-09-02 ENG 1(2) OIL FILTER CLOG Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.03

79-20-02 EMCD Visual Pop- Out Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.04

79-40-01 Fuel Return Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.04


A320/321MEL/CDL

12 FEB 12MEL

7/23/2019 A 320321 Mel Cdl


ATA 80 - STARTING

80-01-31 ENG MAN START pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.0

80-07-01 Start Valve Position Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . 01.80.0

80-11-01 Start Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.0

80-12-01 FAULT light on the ENG MASTER Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.0

* * *

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FAA MMEL Preamble

The following is applicable for authorized certificateholders operating under Federal Aviation Regulations

(FAR) Parts 121, 125, 129, 135: The FAR require that allequipment installed on an aircraft in compliance with the

Airwor thiness Standards and the Operating Rules mustbe operative. However, the Rules also permit thepublication of a Minimum Equipment List (MEL) wherecompliance with certain equipment requirements is notnecessary in the interests of safety under all operatingconditions. Experience has shown that with the variouslevels of redundancy designed into aircraft, operation of every system or installed component may not benecessary when the remaining operative equipment canpr ovi de an acceptable l evel of safet y. A Mast er Minimum Equipment List (MMEL) is developed by the

FAA, with participation by the aviation industry, toimprove aircraft utilization and thereby provide moreconvenient and economic air transportation for thepublic. The FAA approved MMEL includes those itemsof equipment related to airworthiness and operatingregulations and other items of equipment which the

Administrator f inds may be inoperative and yet maintainan acceptable level of safety by appropriate conditionsand limitations; it does not contain obviously requireditems such as wings, flaps, and rudders. The MMEL isthe basis for development of individual operator MELswhich take into consideration the operator’s particular aircraft equipment configuration and operational

conditions. Operator MELs, for administrative control,may include items not contained in the MMEL; however,relief for administrative control items must be approvedby the Administrator. An operator’s MEL may differ informat from the MMEL, but cannot be less restrictivethan the MMEL. The individual operator’s MEL, whenapproved and authorized, permits operation of theaircraft with inoperative equipment.

E quipment not r equi r ed by t he oper at i on bei ngc o n d u c t e d a n d e q u i p m e n t i n e x c e s s o f F A Rrequirements are included in the MEL with appropriateconditions and limitations. The MEL must not deviate

from the Aircraft Flight Manual Limitations, EmergencyProcedures or with Airworthiness Directives. It isimportant to remember that all equipment related to theairworthiness and the operating regulations of theaircraft not listed on the MMEL must be operative.

Suitable conditions and limitations in the formplacards, maintenance procedures, crew operatprocedures and other restrictions as necessary a

specified in the MEL to ensure that an acceptable leof safety is maintained.

T h e M E L i s i n t e n d e d t o p e r m i t o p e r a t i o n winoperative items of equipment for a period of time urepairs can be accomplished. It is important that repabe accomplished at the earliest opportunity. In ordemaintain an acceptable level of safety and reliability MMEL establishes limitations on the duration of aconditions for operation with inoperative equipmeThe MEL provides forreleaseof theaircraft forflight winoperative equipment. When an item of equipmendiscovered to be inoperative, it is reported by making

entry in the Aircraft Maintenance Record/Logbookprescribed by FAR. The item is then either repairedmay be deferred per the MEL or other approved meaaccept abl e t o t he A dmini str at or pr i or t o f ur thoperation. MEL conditions and limitations, do not reliethe operator from determining that the aircraft iscondition for safe operation with items of equipminoperative.

When these requirements are met, an AirworthineRelease, Aircraft Maintenance Record/Logbook eno r o t h e r a p p r o v e d d o c u m e n t a t i o n i s i s s u e d prescribed by FAR. Such documentation is requi

p r i o r t o o p e r a t i o n w i t h a n y i t e m o f e q u i p m einoperative.

Operators are responsible for exercising the necessoperational control to ensure that an acceptable levesafety is maintained. When operating with multiinoperative items, the interrelationships between thoitems and the effect on aircraft operation and crworkload will be considered.

Operators are to establish a controlled and sound repprogram including the parts, personnel, facilitiprocedures, and schedules to ensure timely repair.

WHEN USING THE MEL, COMPLIANCE WITH TSTATED INTENT OF THE PREAMBLE, DEFINITION

A N D T H E C O N D I T I O N S A N D L I M I T A T I OSPECIFIED IN THE MEL IS REQUIRED.

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Definitions

1. System Definitions.

System numbers are based on the Air Transport Association (ATA) Specification Number 100 anditems are numbered sequentially.

a. “SYSTEM & SEQUENCE NUMBERS - ITEM”(Column 1) means the equipment, system,component, or function listed in the “Item” column.The letters “SV” added at the end of a sequencenumber indicates that it is a Saudia added itemand will not be found in the FAA Master MEL.Where applicable, EICAS/EIS status message(s)are also listed in this column..

b. “NUMBER INSTALLED” (Column 2) is thenumber (quantity) of items normally installedin theaircraft. This number represents the aircraftconfiguration considered in developing the MEL.Should the number be a variable (e.g., passenger cabin items) a number is not required, are a dash(-) symbol is shown.

c. “ N U MB E R R E Q U IR E D F O R D I S P A TC H ”(Column 3) is the minimum number (quantity) of i tems required for operation provided theconditions specified in Column 4 are met.

NOTE:

Where the MMEL shows a variable number required for dispatch, the MEL must reflectthe actual number required fordispatch or analternate means of configuration controlapproved by the Presidency of Civil Aviation(PCA).

d “REMARKS OR EXCEPTIONS” (Column 4) thiscolumn includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions andlimitations) for such operation, and appropriatenotes.

e. A vertical bar (change bar) in the margin indicatesa change, addition or deletion in the adjacent textfor the current revision of that page only. Thechange bar is dropped at the next revision of thatpage.

2. “Airplane Flight Manual” (AFM) is the documentrequired for type certification and approved by the

responsible FAA Aircraft Certification Office. The FAAapproved AFM for the specific aircraft is listed on theapplicable Type Certificate Data Sheet. (The AFM willnot be carried aboard the aircraft).

3. “Placarding” Each inoperative item must be placardedt o i nfor m and r emi nd t he cr ewmember s andmaintenance personnel of the equipment condition.placard should be located adjacent to the control or indicator for the item affected, unless otherwisespecified, placard wording and location will bedetermined by the placarding procedures located onsection 3 of this manual.

4. “-” symbol in Column 2 and/or Column 3 indicates avariable number (quantity) of the item installed.

5. “ER” refers to extended range operations of a two-engine airplane which has a type design approval for ER operations and complies with the provisions of

Advisory Circular 120-42A.

6. “Extended over-water operation” means operationover water at a horizontal distance of more than 50nautical miles from the nearest shoreline.

7. “Federal Aviation Regulations” (FAR) means theapplicable portions of the Federal Aviation Act andFederal Aviation Regulations.

8. “Flight” for MEL purposes means one operationalcycle of the aircraft including only one takeoff and onelanding. Where a proviso includes a limitation on thenumber of flights permitted with an inoperative item,the count will start with the next flight after discoverythat the item has become inoperative.

9. “Flight Hours” for MEL purposes means the time fromthe moment the aircraft leaves the surface of the earthuntil it touches down at the next point of landing (i.e.,takeoff to landing time). “Flight Hours” is identical to

“time in service,” as defined by GACA/FAR Part 1.Where a proviso includes a limitation on the number of flight hours permitted with an inoperative item, the timewill start at the next takeoff after discovery that the itemhas become inoperative.

10. “Flight Day” means a 24 hour period (from midnight tomidnight) Universal Coordinated Time (UCT), duringwhich at least one flight is initiated for the affectedaircraft.

01.01.02MEL INTRODUCTION


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Definitions (Cont’d)

11. “Icing Conditions” meansan atmospheric environment

that may cause ice to form on the aircraft or in theengine(s).

12. “Inoperative” means a system and/or componentmalfunction to the extent that it does not accomplish itsi nt ended pur pose and/ or i s not consi st ent l yfunctioning normally within its approved operatinglimit(s) or tolerance(s).

13. “NOTES:” in Column 4 provides additional informationfor crewmember or maintenance consideration. Notesare used to identify applicable material which isintended to assist with compliance, but do not relievethe operator of the responsibility for compliance with

all applicable requirements.

14. “Inoperative components of an inoperative system”:Inoperative items which are components of a systemw hi ch i s i noper at ive ar e usuall y consider edcomponents directly associated with and having noo t h er f u nc t io n t h an t o s u p po r t t h a t s y s te m .(Warning/caution systems associated with theinoperative system must be operative unless relief isspecifically authorized per the MEL).

15. “(M)” symbol indicates a requirement for a specificmaintenance procedure which must be accomplishedprior to operation with the listed item inoperative.Normally these procedures are accomplished bymaintenance personnel; however, other personnelmay be qualified and authorized to perform certainf unct i ons. P r ocedur es r equi r i ng speci al i zedknowledge or skill, or requiring the use of tools or testequipment should be accomplished by maintenancepersonnel. The satisfactory accomplishment of allmaintenance procedures, regardless of who performsthem, is the responsibility of Technical Services.

Appropriate procedures are required to be publishedas part of Technical Services manuals or MEL.

16. “(O)” symbol indicates a requirement for a specific

operations procedure which must be accomplished inplanning for and/or operating with the listed itemi noper at i ve. N or mal l y t hese pr ocedur es ar eaccomplished by the flight crew; however, other personnel may be qualified and authorized to performcertain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, isthe responsibility of Flight Operations. Appropriateprocedures are required to be published as a part of Flight Operations manuals or MEL.

NOTES:

The (M) and (O) symbols are required in Saudi Ar ab ia n Ai rL in es ME L un le ss ot he rw is eauthorized by the GACA.

17. “Deactivated” and “Secured” means that the specifcomponent must be put into an acceptable conditfor safe flight. An acceptable method of securingdeactivating willbe established by Technical Servic

18. “Visual Flight Rules” (VFR) is as defined in FAR P91. This precludes a pilot from filing an InstrumFlight Rules (IFR) flight plan.

19. “Visual Meteorological Conditions” (VMC) means atmospheric environment is such that would allowflight to proceed under the visual flight rules applicato the flight. This does not preclude operating undInstrument Flight Rules.

20. “Visible Moisture” means an atmospheric environmcontaining water in any form that can be seennatural or artificial light; for example, clouds, fog, rasleet, hail, or snow.

21. “Passenger Convenience Items” , Deleted, See N32.

22. “Non-combustible materials” means metallic objethat will not sustain a fire.

23. “ R e p a ir ” a n d “ R e p l a ce m e n t ” r e f e r t o s u

maintenance action as necessary to restore inoperative item to an operative condition.

24. “Crewmember “ means a person assigned to perfoduty in an aircraft during flight time.

25. Repair Intervals: All users of an MEL approved unFAR 121, 125, 129 and 135 must effect repairsinoperative systems or components, deferredaccordance with the MEL, at or prior to the repair timestablished by the following letter designators:

Category A. Items in this category shall be repai

within the time interval specified in

remarks column of the operato

approved MEL.

Category B. Items in this category shall be repai

within three (3) consecutive calen

days (72 hours), excluding the day th


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malfunction was recorded in the aircraft

maintenance record/logbook. For

example, if it were recorded at 1000

UCT on January 26th, the three day

interval would begin at midnight the 26thand end at midnight the 29th.

Category C. Items in this category shall be repaired

within ten (10) consecutive calendar

days (240 hours), excluding the day the


maintenance record/logbook. For

example, if it were recorded at 1000

UCT on January 26th, the 10 day

interval would begin at midnight the 26th

and end at midnight February 5th.

Category D. Items in this category shall be repairedw i t hi n one hundr ed t w ent y ( 120)

consecutive calendar days (2880

h o ur s) , e x cl ud in g t he d a y t he


maintenance record/logbook.

The letter designators are inserted adjacent toColumn 2.

26. Electronic Fault Alerting System - General

New generation aircraft display system faultindications to the flight crew by use of computerized

display systems. Each aircraft manufacturer hasincorporated individual design philosophies indetermining the data that would be represented. Thefollowing customized definition may be used to helpdetermine the level of messages affectingthe aircraft’sdispatch status.

a. AIRBUS (A320, A321, A330)

Airbus aircraft equipped with Electronic Centralized

Aircraft Monitoring (ECAM) provide different levels

of system condition messages (WARNING,

CAUTION, STATUS and ADVISORY). A-320/321

and A-330 also provide MAINTENANCE status

messages.

Any message that affects airplane distpatchability

will normally be at the WARNING, CAUTION or

STATUS level. MAINTENANCE messages (A-

320/321 and A-330 only) are also indicated on

ECAM Status Page below the white Maintenance

label.

A MAINTENANCE status (Class II) message on

ECAM indicates the presence of a system fault

which can be identified by CFDS (A-320/321) or

CMS (A-330) interrogation. The systems are

designed to be fault tolerant; however for any

MAINTENANCE status (ClassII) message the A-3120/321 MEL must be verified for dispatch

capability. For the A-330, MAINTENANCE status

messages do not affect dispatch.

b. BOEING (B-747-468, B-777)

Boeing aircraft equipped with Engine Indicating and

Crew Alerting Systems (EICAS), provide different

priority levels of system messages (WARNING,

C AU TI ON , A DV IS OR Y, S TA TU S a nd

MAINTENANCE). Any messages that affects

aircraft dispatch status will be displayed as a

STATUS message level or higher. The absence of

an EICAS STATUS or higher level (WARNING,CAUTION, ADVISORY) message indicates that the

system/component is operating within its approved

operating limits or tolerances.

System conditions that result only in a maintenance

level message, i.e., no correlation with a higher

level EICAS message, do not affect dispatch and do

not require action other than as addressed within an

operator’s standard maintenance program.

c. DOUGLAS (MD-11, MD-90)

Some Douglas aircraft are equipped with an

alerting function which is a subsystem within the

Electronic Instrument System (EIS). The alertingfunction provides various levels of system condition

alerts (WARNING, CAUTION, ADVISORY,

MAINTENANCE and STATUS).

Alerts that affect aircraft dispatch will include

WA RN I NG , C AU TI O N, S TA TU S o r

MAINTENANCE level. MAINTENANCE alerts are

displayed on the status page of the EIS display

panel under the maintenance heading.

A MAINTENANCE alert on the EIS indicates the

presence of a system fault which can be identified

by the Central Fault Display System (CFDS for MD-

11), or Engine and Alert Display (EAD for MD-90)interrogation. The systems are designed to be fault

tolerant, however, for any MAINTENANCE alert,

the MEL must be verified for dispatch purposes.




MEL

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d. EMBRAER ( ERJ-170)

The ERJ-170 are equipped with an Engine

indicating and crew alerting system (EICAS) that

provides three different message levels :

WARNING,CAUTION, and ADVISORY. The ERJ -

170 SERIES and STATUS messages. Failures that

effect dispatchability are presented to the flight

crew at one of these levels.other failures may be

presentes only to the maintenance personnel on

the multi function display (MFD) maintenance

pages or through the download of the Central

Maintenance Computer (CMC).

26. System conditions that result only in a maintenance

level message, I.e. No correlation with a higher levelEICAS message, do not affect dispatch and do notrequire action other than as addressed within anoperator’s standard maintenance program.

27. “ D a y o f D i s co v e r y ” i s t h e c a l e n da r d a y a nequipment/instrument malfunction was recorded inthe aircraft maintenance log and/or record. This day isexcluded from the calendar days or flight daysspecified in the MEL for the repair of an inoperativeitem of equipment. This provision is applicable to allMEL items, i.e., categories “A, B, C, and D.”

28. “Operative” or “Operates normally” - When the MEL

specifies that an item of equipment is operative or thatit operates normally, it means that the system and/or component will accomplish its intended purpose and isconsistently functioning normally within its designoperating limit(s) and tolerance(s). It does not meanthat its operational status must be verified; it is to beconsidered operativeunlessreportedor is known to bemalfunctioning.

29. “Must be verified operative” or “Must be verified tooperate normally”- When the MEL specifies that anitem of equipment must be verified operative, it meansthat it must be checked and confirmed operative at theinterval(s) specified for the item. When the MEL

specifies that an item of equipment must be verifiedoperative, but no interval is specified, verification isrequired only at the time of deferral.

30. A “(FD)” symbol indicates a requirement for thetechnical personnel to notify flight dispatch as soon asa relevant MEL item becomes open on the hold itemlist and must be shown on the flight dispatch release,or an amendment made. Such items normally involve

restrictions associated with flight level, speed, weigetc.

31. “Considered inoperative”,as used in the provismeans that item must be treated for dispatch, taxi a

flight purposes as though it were inoperative. The itshall not be used or operated until the original deferi t em i s r epair ed. A ddit i onal act ions i ncludocumenting the item on the dispatch releaseapplicable), placarding, and complying with remarks, exceptions, and related MMEL provisioincluding any (M) and (O) procedures and observthe repaircategory.

32. Nonessential equipment and furnishings (NEF) those items installed on the aircraft as part of original certification,supplemental type certificateengineering order that have no effect on the s

operation of flight and would not be required by applicable certification rules or operational rules. Thare those item that if inoperative, damaged or misshave no effect on the aircraft’s ability to be operatsafely under all operational conditions.

Weight Reductions

The MEL weight reductions must be applied to maximum performance limited weights, as follows:

1. Takeoff - Weight penalty is applied to the m

restrective of the Zero Wind weight

Climb Limit weight.

2. Enroute - Weight penalty is applied to cruise a

o n e e n g i n e i n o p e r a t i v e A l t i t u

Capability limited weights.

3. Landing - Weight penalty is applied to the m

restrective of tailored landing cha

field length or landing climb limi

weight.

Dispatch Fuel Penalty

The percentage increase in the fuel must be appliedthe minimum dispatch fuel requirement.

Minimum dispatch fuel required is the sum of trip fualternate fuel and reserve fuel.

* * *

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A320/321MEL/CDL

MEL


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ECAM WARNINGS / MEL ENTRY

The following pages give correspondence between ACAM caution/warning messages and MEL item number:

CAUTION

1) This section is, normally, not intended to cover false cautions/warnings.

However, if a caution/warning is determined to be false by troubleshooting, the crew should refer to the concerne

caution/warning message item (if listed) in the associated ATA chapter 01.

2) In order to help the crew to determine the MEL ENTRY point corresponding to a caution/warning message, the

REMARK column contains the text:

a) “Actual warning” or “Actual caution”.The associated MEL item number is the MEL ENTRY point which gives the dispatch conditions correspondin

to an actual failure of the system/ component monitored by the caution/warning.

b) “False warning” or “False caution”.

The associated MEL item number is the MEL ENTRY point which gives the dispatch conditions correspondin

to the failure of the warning, determined by troubleshooting. The system/component monitored by the

caution/warning being still operative.

3) When the REMARK column contains neither, “Actual caution/warning”, nor “False caution/warning” textes, the ME

ENTRY point corresponds to an actual warning which indicates an actual failure of the system/component monitored

the caution/warning.

4) When either an actual, or a false caution/warning is activated, this section gives the MEL ENTRY point to be

considered.

But the crew MUST CHECK THAT THE AIRCRAFT SYSTEMS/COMPONENTS ARE IN A CONDITION WHCIH

COMPLIES WITH THE DISPTACH CONDITIONS.

IF NOT, AIRCRAFT DISPATCH IS NOT ALLOWED.

5) When a caution/warning is associated with the wording “Not applicable” in the Display Condition column, this mean

that the MEL is not appropriate document to be consulted.

When such caution/warnins have been triggered, application of associated procedure, if any , (refer to FCOM

Abnormal/Emergency procedures), and/or accomplishment of maintenance action, if required, would permit to fix theproblem.

( Cont'd on next page )

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ECAM WARNINGS / MEL ENTRY ( Cont'd )

ECAM

The A320/321 Family aircraft is equipped with Electronic Centralized Aircraft Monitoring (ECAM) which provides

different levels of aircraft systems monitoring messages:

- ECAM warning. - ECAM advisory. - ECAM caution. -ECAM memo.

ECAM warning and ECAM caution messages are listed in the “MEL Entries” section.

ECAM advisory and ECAM memo messages are not listed in the “MEL Entries” section.

CONDITION OF DISPATCH COLUMN

- NO DISPATCH: It is not permitted to dispatch the aircraft when the ECAM displays this alert.

- NOT APPLICABLE: The ECAM alert does not report a system failure and is not related to MEL. The MEL shall not be

used.

This is not a NO-GO situation. The corrective action to revert to normal condition is immediate, obvious or well known

by flight crew and/or maintenance personnel.

EXAMPLES

1) If the “BAT FAULT” caution message is displayed on ECAM, the crew must refer to MEL 24-30-02 (Battery channel).

2) If the “ac bus 1 fault fault” CAUTION MESSAGE IS DISPLAYED ON ecam, a/c DISPATCH IS NOT ALLOWED.

3) If the “GEN 1 OFF” caution message is displayed on ECAM no MEL entry is required, and the text “Not applicable” is

written in the Remark column.

In this example, the crew must switch on the generator pb sw.

4) If ”PACK 1 + 2 FAULT” caution message is displayed the crew must refer to FCOM for “FLIGHT WITHOUT

PRESURIZATION”.

Note : The ECAM warnings and cautions listed in section 00E in the column “ECAM WARNINGS” are generic.

*example :

ECAM WARNING DISPATCH CONDITION REMARK

FCU 1(2) (1 + 2) FAULT Refer to MEL 22-81-01

Wording FCU 1(2) (1 + 2) FAULT represents the three messages ; “FCU 1 FAULT” “FCU 2 FAULT” “FCU 1 + 2

FAULT”.

* * *

01.02.02GENERAL


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ATA 21 AIR CONDITIONING

ECAM WARNING ACTION DISPATCH CONDITION

AIR

AFT CRG VENT FAULT Refer to MEL 21-28-03

COND CTL 1(2)-A(B) Refer to MEL 21-63-04

PACK 1(2) FAULT Refer to MEL 21-52-01

PACK 1+ 2 FAULT Refer to FCOM/PRO-SPO-20

PACK 1(2) OFF Refer to MEL 21-52-01

PACK 1(2) OVHT Refer to MEL 21-52-01

PACK 1 (2) REGUL FAULT Refer to MEL 21-27-01-01 If pack outlet temperature is

affected

Refer to MEL 21-07-01-03 If pack compressor outlet

temperature is affected

Refer to MEL 21-51-03 If pack flow sensor is affecte

Refer to MEL 21-52-01 If pack flow control valve is

affected

Refer to MEL 21-52-02 If pack ram air inlet is affecte

Refer to MEL 21-61-01 If turbine bypass valve

affected

CAB PR

EXCESS CAB ALT Not applicable

EXCESS RESIDUAL PR Apply ECAM procedure

LDG ELEV FAULT Refer to MEL 21-31-04

LO DIFF PR Not applicable

OFV NOT OPEN NO DISPATCH

SAFETY VALVE OPEN Refer to FCOM/PRO-SPO-20 Actual alert

Refer to MEL 21-09-03 False alert

SYS 1(2) FAULT Refer to MEL 21-31-01

SYS 1+2 FAULT Refer to FCOM/PRO-SPO-20

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COND

AFT CAB DUCT OVHT Refer to MEL 21-63-02

AFT CARGO DUCT OVHT Refer to MEL 21-43-02

AFT CRG HEAT FAULT Refer to MEL 21-43-02

AFT CRG ISOL VALVE Refer to MEL 21-28-04

CKPT DUCT OVHT Refer to MEL 21-63-02

FWD CAB DUCT OVHT Refer to MEL 21-63-02

HOT AIR FAULT Refer to MEL 21-63-03

L + R CAB FAN FAULT NO DISPATCH

LAV + GALLEY FAN FAULT Refer to MEL 21-23-01

TRIM AIR SYS FAULT Not applicable If the trim air valves are colsed

Refer to MEL 21-63-02 If the associated AFT CAB

TRIM VALVE message is

displayed

Refer to MEL 21-63-02 If the associated FWD CAB

TRIM VALVE message is

displayed

Refer to MEL 21-63-02 If the associated CKPT TRIM

VALVE message is displayed

Refer to MEL 21-63-02 If the associated TRIM AIR HI

PR message is displayed

VENT

AVNCS SYS FAULT Refer to MEL 21-26-04 If the VENT SKIN VALVE

FAULT alert is displayed on the

EWD.

Refer to MEL 21-26-05 If the VENT SKIN VALVE


EWD.

Refer to MEL 21-26-03, or



Refer to MEL 21-26-10

01.03.02ECAM MESSAGES

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VENT

BLOWER FAULT Refer to MEL 21-26-01 Actual caution

Refer to MEL 21-09-01 False caution

EXTRACT FAULT Refer to MEL 21-26-02 Actual caution


SKIN VALVE FAULT Refer to MEL 21-26-04 Faulty valve

determined on the

CAB PRESS page


ATA 22 AUTO FLIGHT


AUTO FLT

A/THR LIMITED Not applicable

A/THR OFF Refer to MEL 22-30-01 Actual caution


AP OFF Refer to MEL 22-10-01 Actual warning

Refer to MEL 22-10-06 False warning

FAC 1 FAULT Refer to MEL 22-60-01

FAC 2 FAULT Refer to MEL 22-60-02

FAC 1 + 2 FAULT NO DISPATCH

FCU 1 (2) FAULT Refer to MEL 22-81-03-01

FCU 1 + 2 FAULT NO DISPATCH

REAC W/S DET FAULT (if installed) Refer to MEL 22-60-03

RUD TRIM 1 (2) FAULT Refer to MEL 27-22-01

RUD TRIM SYS NO DISPATCH

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ATA 22 AUTO FLIGHT


AUTO FLT

RUD TRV LIM 1 (2) Refer to MEL 27-23-01

RUD TRV LIM SYS NO DISPATCH

YAW DAMPER 1 (2) Refer to MEL 22-60-04

YAW DAMPER SYS NO DISPATCH

WINDSHEAR

DET FAULT Refer to MEL 22-60-03

ATA 23 COMMUNICATIONS


COM

ACARS FAULT (If installed) Refer to MEL 46-21-01

CIDS 1 + 2 FAULT NO DISPATCH

HF 1 (2) DATA FAULT (If installed) Refer to MEL 23-10-01

HF 1 (2) EMITTING (If installed) Refer to MEL 23-51-03 If hand microphone

selector is jammed in

the transmitting

position

Refer to MEL 23-51-06 If side stick radio

selector is jammed in

the transmitting

position

Refer to MEL 23-52-05 If a transmission Key

on one ACP is

jammed in the

transmitting position.


01.03.04EICAM MESSAGES


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ATA 23 COMMUNICATIONS


COM

SATCOM DATA FAULT (If installed) Refer to MEL 23-10-03, and


SATCOM FAULT (If installed) Refer to MEL 23-10-03, and


VHF 3 DATA FAULT Refer to MEL 23-10-02

VHF 1(2)(3) EMITTING Refer to MEL 23-51-03, If hand microphone

selector is jammedthe transmitting

position

Refer to MEL 23-51-06 If side stick radio

selector is jammed

the transmitting

position

Refer to MEL 23-52-05 If a transmission K

on one ACP is

jammed in the

transmitting positio


ATA 24 ELECTRICAL POWER


C/B

TRIPPED Refer to affected systems Actual alert


12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 24 ELECTRICAL POWER


ELEC

AC BUS 1 FAULT NO DISPATCH

AC BUS 2 FAULT NO DISPATCH

AC ESS BUS ALTN NO DISPATCH

AC ESS BUS FAULT NO DISPATCH

AC ESS BUS SHED NO DISPATCH Actual caution


APU GEN FAULT Refer to MEL 24-23-01

BAT 1(2) FAULT NO DISPATCH

BAT 1 (2) OFF Not applicable

BCL 1 (2) FAULT Refer to MEL 24-38-02 Actual caution

DC BAT BUS FAULT NO DISPATCH

DC BUS 1 + 2 FAULT NO DISPATCH

DC BUS 1 FAULT NO DISPATCH

DC BUS 2 FAULT NO DISPATCH

DC EMER CONFIG NO DISPATCH

DC ESS BUS FAULT NO DISPATCHDC ESS BUS SHED NO DISPATCH

EMER CONFIG NO DISPATCH

EMER GEN 1 LINE OFF Not applicable

ESS BUSSES ON BAT NO DISPATCH

ESS TR FAULT Refer to MEL 24-34-01

GEN 1 (2) FAULT Refer to MEL 24-22-01

GEN 1 (2) OFF Not applicable

GEN 1 (2) (APU GEN) OVERLOAD Refer to MEL 24-26-01

IDG DISCONNECTED Refer to MEL 24-22-01

IDG 1 (2) OIL LO PR Refer to MEL 24-22-01

IDG 1 (2) OIL OVHT Refer to MEL 24-22-01

STATIC INV FAULT NO DISPATCH

TR 1 (2) FAULT Refer to MEL 24-32-01



MEL

7/23/2019 A 320321 Mel Cdl


ATA 26 FIRE PROTECTION


APU FIRE NO DISPATCH Actual alert


APU

FIRE DET FAULT Refer to MEL 26-13-01, and


FIRE LOOP A(B) FAULT Refer to MEL 26-13-01 If loop A is failed

Refer to MEL 26-13-02 If loop B is failed

AVIONICS SMOKE NO DISPATCHr Actual alert


ENG 1(2)FIRE NO DISPATCH

ENG 1(2)

FIRE DET FAULT NO DISPATCH

FIRE LOOP A FAULT Refer to MEL 26-12-01 If engine 1 is affected

Refer to MEL 26-12-02 If engine 2 is affected

FIRE LOOP B FAULT Refer to MEL 26-12-03 If engine 1 is affected

Refer to MEL 26-12-04 If engine 2 is affected

SMOKE

AFT CARGO SMOKE NO DISPATCH Actaual alert


AFT CRG BTL FAULT Refer to MEL 26-23-02 If the SMOKE FWD CRG BT

FAULT alert is not displayed

on the EWDRefer to MEL 26-23-01 If the SMOKE FWD CRG BT

FAULT alert is displayed on

the EWD

AFT CRG DET FAULT Refer to MEL 26-16-02

12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 26 FIRE PROTECTION


SMOKE

FWD CARGO SMOKE NO DISPATCH Actual alert


FWD CRG BTL FAULT Refer to MEL 26-23-02 If the SMOKE AFT CRG BTL

FAULT alert is not displayed on

the EWD

Refer to MEL 26-23-01 If the SMOKE AFT CRG BTL


EWD

FWD CRG DET FAULT Refer to MEL 26-16-01

DET FAULT Refer to MEL 23-73-10-01

LAVATORY DET FAULT Refer to MEL 26-17-01

LAVATORY SMOKE NO DISPATCH Actual alert


ATA 27 FLIGHT CONTROLS


CONFIG

L(R) SIDESTICK FAULT NO DISPATCH

PITCH TRIM NOT IN T.O. RANGE NO DISPATCH

RUD TRIM NOT IN T.O. RANGE NO DISPATCH

SLATS (FLAPS) NOT IN T.O. CONFIG NO DISPATCH

SPEED BRK NOT RETRACTED NO DISPATCH



MEL

7/23/2019 A 320321 Mel Cdl




F/CTL

AIL SERVO FAULT Refer to MEL 27-14-01, or




ALTN LAW NO DISPATCH

DIRECT LAW NO DISPATCH

ELAC 1 FAULT Refer to MEL 27-93-01

ELAC 1 PITCH FAULT Refer to MEL 27-93-01

ELAC 2 FAULT NO DISPATCH

ELAC 2 PITCH FAULT NO DISPATCH

ELEV SERVO FAULT NO DISPATCH If servocontrol is affected

Refer to MEL 27-34-02 If servocontrol position

transducer is affected

FCDC 1 FAULT NO DISPATCH

FCDC 2 FAULT Refer to MEL 27-95-02

FCDC 1+2 FAULT NO DISPATCH

FLAP ATTACH SENSOR NO DISPATCHFLAP LVR NOT ZERO Not applicable

FLAP SYS 1 FAULT NO DISPATCH

Refer to MEL 27-54-01 If the maintenance confirms

that the F/CTL FLAP SYS 1


the EWD due to a flap motor

failure

FLAP SYS 2 FAULT Refer to MEL 27-51-01

Refer to MEL 27-54-01 If the maintenance confirms

that the FTCL FLAP SYS 2


the EWD due to a flap motor

failure.

FLAP TIP BRK FAULT Refer to MEL 27-51-03

FLAPS (SLATS) FAULT NO DISPATCH

12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl




F/CTL

FLAPS (SLATS) LOCKED NO DISPATCH

GND SPLR FAULT Refer to MEL 32-42-06 If the braking system is affected

Refer to MEL 27-92-02 If the braking system is not

affected

GND SPLR (1 + 2)(3 + 4) FAULT Refer to MEL 27-92-02

L(R) AIL FAULT NO DISPATCH

L(R) ELEV FAULT NO DISPATCH

L + R ELEV FAULT NO DISPATCH

L(R) SIDESTICK FAULT NO DISPATCH

SEC 1 FAULT Refer to MEL 27-94-01



SIDESTICK PRIORITY Refer to FCOM/PRO-ABN-27

SLAT SYS 1 FAULT NO DISPATCH

Refer to MEL 27-84-01 If the maintenance confirms the

F/CTL SLAT SYS 1 FAULT

alert is displayed on the EWDdue to a slat motor failure.

SLAT SYS 2 FAULT Refer to MEL 27-51-02

Refer to MEL 27-84-01 If the maintenance confirms the

F/CTL SLAT SYS 2 FAULT

alert is displayed on the EWD

due to a slat motor failure.

SLAT TIP BRK FAULT Refer to MEL 27-81-01

SPD BRK DISAGREE Refer to MEL 27-92-01

SPD BRK FAULT Refer to MEL 27-92-01

SPD BRK STILL OUT Not applicable

SPD BRK 2(3 + 4) FAULT Refer to MEL 27-92-01



MEL

7/23/2019 A 320321 Mel Cdl




F/CTL

SPLR FAULT Refer to MEL 27-64-01,

Refer to MEL 27-64-02,

Refer to MEL 27-64-03,



STABILIZER JAM NO DISPTACH

ATA 28 FUEL


FUEL

ACT PUMP LO PR Refer to MEL 28-28-03

ACT UNUSABLE Not applicable

ACT XFR FAULT Refer to MEL 28-12-05, or Actual alert










APU LP VALVE FAULT Refer to MEL 28-29-01

AUTO FEED FAULT Refer to MEL 28-20-01

AUTO TRANSFER FAULT Refer to MEL 28-26-01

12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 28 FUEL


FUEL

CTR TK PUMP 1(2) LO PR Refer to MEL 28-21-02

CTR TK PUMPS LO PR Refer to MEL 28-21-02

CTR TK PUMPS OFF Not applicable

CTR TK XFR OFF Not applicable

ENG 1(2) LP VALVE OPEN Refer to MEL 28-24-01

FQI CH 1(2) FAULT Refer to MEL 28-50-01

F.USED/FOB DISAGREE Not applicable

L(R) INNER (OUTER) TK HI TEMP Disptach possible only if

“delay T.O.” is not displayed

on ECAM

Actual alert


L(R) WING TK HI TEMP Disptach possible only if

“delay T.O.” is not displayed

on ECAM

Actual alert


L(R) INNER (OUTER) TK LO TEMP NO DISPATCH Actual alert

Refer to MEL 28-09-02 False alertL(R) WING TK LO TEMP NO DISPATCH Actual alert


L(R) TK PUMP 1(2) LO PR Refer to MEL 28-21-01

L(R) TK PUMP 1 + 2 LO PR NO DISPATCH

L(R) WING TK LO LVL NO DISPATCH Actual alert


L+R WING TK LO LVL NO DISPATCH

L(R) WING TK OVERFLOW NO DISPATCH

L(R) XFR VALVE CLOSED or OPEN Refer to MEL 28-15-01, or


L(R) XFR VALVE FAULT Refer to MEL 28-21-02

X FEED VALVE FAULT NO DISPATCH

XFR VALVES FAULT Refer to MEL 28-21-02



MEL

7/23/2019 A 320321 Mel Cdl


ATA 29 HYDRAULIC POWER


HYD

B ELEC PUMP LO PR NO DISPATCH Actual caution


B ELEC PUMP OVHT NO DISPATCH Actual caution


B RSVR LO AIR PR NO DISPATCH Actual caution


B RSVR LO LVL NO DISPATCH Actual caution


B RSVR OVHT NO DISPATCH Actual caution


B SYS LO PR NO DISPATCH Actual caution


B + G SYS LO PR NO DISPATCH Actual warning


B + Y SYS LO PR NO DISPATCH Actual warning


G ENG 1 PUMP LO PR NO DISPATCH Actual caution


G RSVR LO AIR PR NO DISPATCH Actual caution


G RSVR LO LVL NO DISPATCH Actual alert


G RSVR OVHT NO DISPATCH Actual caution


G SYS LO PR NO DISPATCH Actual caution


G + Y SYS LO PR NO DISPATCH Actual warning


12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 29 HYDRAULIC POWER


HYD

PTU FAULT NO DISPATCH Actual caution


RAT FAULT NO DISPTACH Actual caution


Y ELEC PUMP LO PR Refer to MEL 29-24-01 Actual caution


Y ELEC PUMP OVHT Refer to MEL 29-24-01 Actual alert


Y ENG 2 PUMP LO PR NO DISPATCH Actual caution


Y RSVR LO AIR PR NO DISPATCH Actual caution


Y RSVR LO LVL NO DISPATCH Actual caution


Y RSVR OVHT NO DISPATCH Actual caution


Y SYS LO PR NO DISPATCH Actual caution




MEL

7/23/2019 A 320321 Mel Cdl


ATA 30 ICE AND RAIN PROTECTION


ANTI ICE

ALL PITOT NO DISPATCH

CAPT (F/O) (STBY) AOA Refer to MEL 30-31-04

CAPT (F/0) (STBY) L(R) STAT Refer to MEL 30-31-03

CAPT (F/O) (STBY) PITOT Refer to MEL 30-31-02

CAPT + F/O PITOT NO DISPATCH

CAPT + STBY PITOT NO DISPATCH

CAPT (F/O) (STBY) PROBES Refer to MEL 30-31-01

CAPT (F/O) TAT Refer to MEL 30-31-05

DETECT FAULT Refer to MEL 30-81-01

ENG 1(2) VALVE CLSD or OPEN Refer to MEL 30-21-01

F/O + STBY PITOT NO DISPATCH

ICE DETECTED Not applicable

L(R) WINDOW Refer to MEL 30-42-01 If Window Heat Computer

affected


L(R) WINSHIELD Refer to MEL 30-42-01 If Window Heat Computer

affected


L + R WINSHIELD NO DISPATCH

SEVERE

ICE DETECTED Not applicable

WING ANTI ICE

L(R) HI PR Refer to MEL 30-11-01BL(R) VALVE OPEN Refer to MEL 30-11-01

OPEN ON GND Refer to MEL 30-11-01

SYS FAULT Refer to MEL 30-11-01

12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 31 INDICATING/RECORDING SYSTEMS


EIS

DMC 1 FAULT Refer to MEL 31-62-01



FWS

FWC 1 FAULT NO DISPATCH

FWC 2 FAULT Refer to MEL 31-53-01

FWC 1 + 2 FAULT NO DISPATCH

OEB/FWC DISCREPANCY NO DISPATCH

SDAC 1 FAULT NO DISPATCH

SDAC 2 FAULT Refer to MEL 31-55-01

SDAC 1 + 2 FAULT NO DISPATCH

RECORDER

DFDR FAULT Refer to MEL 31-30-03

SYS FAULT Refer to MEL 31-30-05

01.03.16EICAS MESSAGES


MEL

7/23/2019 A 320321 Mel Cdl


ATA 32 LANDING GEAR


BRAKES

ALTN BRK FAULT NO DISPATCH

ALTN L(R) RELEASED NO DISPATCH

A/SKID N/WS FAULT NO DISPATCH

A/SKID N/WS OFF Not applicable

AUTO BRK FAULT Refer to MEL 32-42-05

BRK Y ACCU LO PR NO DISPATCH Actual caution

Refer to MEL 32-44-02 False cautionSYS 1 FAULT Refer to MEL 32-42-03

SYS 2 FAULT Refer to MEL 32-42-04

HOT NO DISPATCH Actual caution


NORM BRK FAULT NO DISPATCH

NORM + ALT FAULT NO DISPATCH

PARK BRK ON Not applicable

RELEASED Refer to MEL 32-42-02 If green brake supply affecte

Refer to MEL 32-42-06 If a tachometer affected

BRAKES-N/WS

MINOR FAULT Refer to MEL 32-09-01

CONFIG

PARK BRK ON NO DISPATCH

L/G

DOORS NOT CLOSED NO DISPATCH

GEAR NOT DOWN Not applicable

GEAR NOT DOWNLOCKED Not applicable

GEAR NOT UPLOCKED Not applicable

GEAR UPLOCK FAULT Refer to MEL 32-31-02

12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 32 LANDING GEAR


L/G

LGCIU 1 FAULT NO DISPATCH

LGCIU 2 FAULT Refer to MEL 32-31-01 If the LGCIU 2 is inoperative

Refer to MEL 32-32-02, or If a RH L/G proximity detector

associated with the LGCIU 2 is

inoperative: apply the relevant

item


Refer to MEL 32-32-08, or Refer to MEL 32-32-11, or


Refer to MEL 32-32-03, or If a LH L/G proximity detector



item





Refer to MEL 32-32-04, or If a Nose L/G proximity detector



item





SHOCK ABSORBER FAULT NO DISPATCHSYS DISAGREE NO DISPATCH



MEL

7/23/2019 A 320321 Mel Cdl


ATA 32 LANDING GEAR


WHEEL

HYD SEL FAULT NO DISPATCH

N/W STRG FAULT Refer to MEL 32-51-01

TYRE LO PR NO DISPATCH Actual caution


ATA 34 NAVIGATION


NAV

ADR 1 FAULT Refer to MEL 34-10-01



ADR (1+2)(1+3)(2+3) FAULT NO DISPATCH

ADR 1+2+3 FAULT NO DISPATCH

ALTI DISCREPANCY Refer to MEL 34-10-01, or



ADR DISAGREE NO DISPATCH

ATT DISCREPANCY Refer to MEL 34-10-04, or




CAPT (F/O)(STBY) AOA FAULT Refer to MEL 34-11-01

FM/GPS POS DISAGREE Not applicable

GPS 1(2) FAULT Refer to MEL 34-50-09

GPWS FAULT Refer to MEL 34-40-01

GPWS TERR DET FAULT Refer to MEL 34-40-01

12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 34 NAVIGATION


NAV

HDG DISCREPANCY Refer to MEL 34-10-04, or




IAS DISCREPANCY Refer to MEL 34-10-01, or

Refer to MEL 34-10-02, or Refer to MEL 34-10-03

ILS 1(2) (1 + 2) FAULT Refer to MEL 34-30-04

IR DISAGREE NO DISPATCH

IR NOT ALIGNED Refer to MEL 34-10-04, or




IR 1 FAULT Refer to MEL 34-10-04

IR 2 FAULT Refer to MEL 34-10-05

IR 3 FAULT Refer to MEL 34-10-06, or


IR (1+2)(1+3)(2+3) FAULT NO DISPATCH

LS 1(2)(1+2) FAULT Refer to MEL 34-30-04

PRED W/S DET FAULT (If installed) Refer to MEL 34-40-06

RA DEGRADED Refer to MEL 34-40-03

RA 1(2) FAULT Refer to MEL 34-40-03

TCAS FAULT Refer to MEL 34-40-04TCAS STANDBY Not applicable

OVERSPEED Not applicable



MEL

7/23/2019 A 320321 Mel Cdl


ATA 36 PNEUMATIC


AIR

APU BLEED FAULT Refer to MEL 36-12-02

APU BLEED LEAK Refer to MEL 36-12-01 Actual caution


BLEED 1(2) OFF Refer to MEL 36-11-01

ENG HP VALVE FAULT Refer to MEL 36-11-07

ENG 1(2) BLEED ABNORM PR Refer to MEL 36-11-01

ENG 1(2) BLEED FAULT Refer to MEL 36-11-01ENG 1(2) BLEED LEAK NO DISPATCH Actual caution


ENG 1(2) (1 + 2) BLEED LO TEMP Refer to MEL 36-11-04

ENG 1(2) BLEED NOT CLSD Refer to MEL 36-11-02

ENG 1(2) LEAK DET FAULT Refer to MEL 36-22-01

L(R) WING LEAK NO DISPATCH

L(R) WING LEAK DET FAULT NO DISPATCH

X BLEED FAULT Refer to MEL 36-12-04

BLEED

MONITORING FAULT NO DISPATCH

MONIT SYS 1(2) FAULT Refer to MEL 36-11-08

12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 46 INFORMATION SYSTEM


DATALINK

ATC FAULT Refer to MEL 46-21-01

ATSU FAULT Refer to MEL 46-21-01

COMPANY FAULT Refer to MEL 46-21-01

ATA 49 AIRBORNE AUXILIARY POWER


APU

AUTO (EMER) SHUT DOWN Refer to MEL 49-10-01

ATA 52 DOORS


DOOR

AFT (BULK) (FWD) CARGO NO DISPTACH Actual caution


L(R) AFT AVIONICS NO DISPATCH Actual caution


L(R) AFT CABIN NO DISPATCH Actual caution


L(R) EMER EXIT (A320) NO DISPATCH Actual caution


L(R) EMER EXIT (A321) NO DISPATCH Actual caution


L(R) FWD AVIONICS NO DISPATCH Actual alert


L(R) FWD CABIN NO DISPATCH Actual caution




MEL

7/23/2019 A 320321 Mel Cdl


ATA 52 DOORS


DOOR

L(R) FWD EMER EXIT (A320) NO DISPATCH Actual alert


L(R) FWD EMER EXIT (A321) NO DISPATCH Actual alert


ATA 70 ENGINE


ENG

COMPRESSOR VANE NO DISPATCH

DUAL FAILURE Not applicable

THR LEVERS NOT SET Refer to MEL 73-20-01

REV SET Not applicable

THRUST LOCKED Not applicable

TYPE DISAGREE NO DISPATCH

VIB SYS FAULT Refer to MEL 77-07-02-05, or

Refer to MEL 77-07-02-06

ENG 1(2)

BLEED STATUS FAULT Apply ECAM procedure If this alert is displayed on th

EWD before the first engine

start, check that no amber

cross is displayed on the EN

SD page for OIL TEMP

indication of the affected

engine. If an amber cross is

displayed, the associated EIUmay be the cause of the

failure (associated engine

start not possible).

12 FEB 12MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl


ATA 70 ENGINE


ENG 1(2)

COMPRESSOR VANE NO DISPATCH

CTL VALVE FAULT NO DISPATCH

EGT (FF)(N1)(N2) DISCREPANCY NO DISPATCH

EIU FAULT NO DISPATCH

FADEC A(B) FAULT NO DISPATCH

FADEC ALTERNATOR NO DISPATCHFADEC FAULT NO DISPATCH

FADEC HI TEMP NO DISPATCH

FAIL Not applicable

FUEL CTL FAULT NO DISPATCH

FUEL FILTER CLOG NO DISPATCH Actual alert


FUEL RETURN VALVE Refer to MEL 73-10-01

HP FUEL VALVE NO DISPATCH

IGN A(B) FAULT Refer to MEL 74-31-01 or

MEL 74-31-02

Actual alert


IGN A+B FAULT NO DISPATCH Actual alert


LOW N1 NO DISPATCH

N1(N2)(EGT) OVER LIMIT Not applicable

OIL FILTER CLOG NO DISPATCH Actual alert


OIL HI TEMP NO DISPATCH

OIL LO PR NO DISPATCH Actual alert


ONE TLA FAULT Refer to MEL 76-11-01


A320/A321MEL/CDL 01 MAY 12

MEL

7/23/2019 A 320321 Mel Cdl


ATA 70 ENGINE


ENG 1(2)

OVSPD PROT FAULT NO DISPATCH

PROBES FAULT

ENG 1(2) REV INHIBITED Refer to MEL 78-30-01

NO DISPATCH

REV ISOL FAULT Refer to MEL 78-30-03

REV PRESSUREIZED NO DISPATCH

REV SWITCH FAULT Refer to MEL 78-30-02

REVERSE UNLOCKED NO DISPATCH

REVERSER FAULT Refer to MEL 78-30-01

SENSOR FAULT NO DISPATCH

SHUT DOWN Not applicable

STALL Not applicable

START FAULT Apply ECAM procedure If the associated THR LEVER

NOT AT IDLE message is

displayed

Refer to FCOM/PRO-SUP-70

START VALVE FAULT Refer to MEL 80-11-01

THR LEVER ABV IDLE Not applicable

THR LEVER DISAGREE NO DISPATCH

THR LEVER FAULT NO DISPATCH

* * *

MEL

A320/A321MEL/CDL 01.03

ECAM MESSAG

7/23/2019 A 320321 Mel Cdl




A320/A321MEL/CDL

MEL

7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-00 MAINTENANCE

Messages on the

STATUS SD page

21-00-03 AFT CRG HEAT

MAINTENANCE

Message

21-00-03A C 1 - AFT CRG HEAT MAINTENANCE message may be

displayed on the STATUS SD page.

21-00-04 TEMP CTL 1(2)

MAINTENANCE

Message

21-00-04A C 2 - TEMP CTL 1(2) MAINTENANCE message may be


21-01 Overhead Panels

21-01-01 AIR COND

Overhead Panel

21-01-01-01 PACK pb-sw

FAULT light

21-01-01-01A C 2 0 One or both may be inoperative provided ECAM BLEED

page displaying system operative.

21-01-01-02 PACK pb-sw

OFF light

21-01-01-02A C 2 0 One or both may be inoperative provided ECAM BLEED

page displaying system operative.

21-01-01-03 HOT AIR pb-swFAULT light

21-01-01-03A C 1 0 May be inoperative provided that all zone duct

temperature indications are operative on the COND SD

page.

12 FEB 12MEL

A320/321MEL/CDL 01.21.01

AIR CONDITIONING

1. 2. NUMBER INSTALLED

SYSTEM & 3. NUMBER REQUIRED FOR DISPATCH

SEQUENCE

OF ITEMS 4. REMARKS OR EXCEPTIONS

I T E M

7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


21-01-01 AIR COND

Overhead Panel

21-01-01-04 HOT AIR pb-sw

OFF light

21-01-01-04A C 1 0 May be inoperative.

21-01-02 CABIN PRESS

Overhead Panel

21-01-02-01 CABIN PRESS

MODE SEL pb-

sw FAULT light


21-01-03 CARGO VENT

Overhead Panel

21-01-03-02 AFT ISOLVALVE pb-sw

FAULT light


21-01-04 VENTILATION

Overhead Panel

21-01-04-01 CAB FANS pb-

sw OFF light




SEQUENCE


I T E M

01.21.02

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


21-01-04 VENTILATION

Overhead Panel

21-01-04-02 BLOWER pb-sw

FAULT light


21-01-04-03 EXTRACT pb-sw

FAULT light


21-07 Indications on SD

pages

21-07-01 Indications on theBLEED SD page

21-07-01-01 Pack Outlet

Temperature

Indication on the

BLEED SD page

21-07-01-01A C 2 0 One or both may be inoperative.

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.03

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


pages

21-07-01 Indications on the

BLEED SD page

21-07-01-02 Pack Turbine

Bypass Valve

Position

Indication on the

BLEED SD page


21-07-01-03 Pack

Compressor

Outlet

Temperature

Indication on the

BLEED SD page


21-07-01-04Pack Flow

Indication on the

BLEED SD page




SEQUENCE


I T E M

01.21.04

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


pages


BLEED SD page

21-07-01-05 Pack Flow

Control Valve

Position

Indication on the

BLEED SD page


21-07-01-06Emergency Ram

Air Inlet Indication

on the BLEED SD

page



CAB PRESS SDpage

21-07-02-01INLET and

EXTRACT

Indications on the

CAB PRESS SD

page


Note:

During ground operations, correctavionics ventilation should be provided.

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.05

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


pages


CAB PRESS SD

page

21-07-02-02 Pressure Safety

Valves Position

Indication on theCAB PRESS SD

page

21-07-02-02A C 1 0 (M) Pressure safety valves may be indicated open provided

that both valves are visually checked closed.

MAINTENACE PROCEDURE

Refer to AMM 21-31-00-040-004

21-07-02-03 Pack 1 and 2

Indications on

the CAB PRESSSD page



COND SD page

21-07-03-01Indications on the

COND SD page

21-07-03-01A C 2 0 One or more indications may be inoperative.


CRUISE SD page

21-07-04-01A C 2 0 Cabin and cockpit zone indications may be inoperative.



SEQUENCE


I T E M

01.21.06

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-09 ECAM Alerts

21-09-01 VENT BLOWER

FAULT Alert

Note:

During ground operations, correct

avionics ventilation should be provided.

21-09-01A Blower fan

operative

C 1 0 (O)(M) May be displayed provided that:

1) The blower fan is checked operative before each flight,

and

2) The VENT AVNCS SYS FAULT alert is checkedoperative before each flight.

OPERATING PROCEDURES

DURING COCKPIT PREPARATION

Disregard the VENT BLOWER FAULT alert displayed on

the EWD.

Disregard the BLOWER pb-sw FAULT light illuminated on

the VENTILATION Overhead Panel.

Note:

If the ground horn sounds:

EIS/HORN/SPLY (121VU P09)

C/B . . . . . . . . . . . . . . . . . . . . . . . . .Pull

The C/B must be closed again after first

engine start

If the ground horn sounds after landing

when engines are off, it can be silenced

again. In this case, the ADIRS must be

set to OFF before leaving the aircraft.


Refer to AMM 21-26-00-040-010

21-09-01B Blower fan

inoperative

C 1 0 May be displayed provided that the avionics blower fan is

considered inoperative.

Refer to Item 21-26-01 Avionics Blower Fan

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.07

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-09 ECAM Alerts

21-09-02 VENT EXTRACT

FAULT Alert

Note:



21-09-02A Extract fan

operative

C 1 0 (O)(M) May be displayed provided that:

1) The extract fan is checked operative before eachflight, and

2) The VENT AVNCS SYS FAULT alert is checkedoperative before each flight.



Disregard the VENT EXTRACT FAULT alert displayed on

the EWD.


Refer to AMM 21-26-00-040-011

21-09-02B Extract fan

inoperative

C 1 0 May be displayed provided that the avionics extract fan is


Refer to Item 21-26-02 Avionics Extract Fan

21-09-03 CAB PR SAFETY

VALVE OPEN

Alert

21-09-03A C 1 0 (M) May be displayed provided that both safety valves are

visually checked closed.


Refer to AMM 21-31-00-040-005



SEQUENCE


I T E M

01.21.08

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-21 Air Distribution

and Recirculation

21-21-01 Cabin Fan

21-21-01A C 2 1 One may be inoperative.

21-23 Lavatory and

Galley Ventilation

21-23-01 Lavatory and

Galley Extraction

Fan

21-23-01B C 1 0 (O) May be inoperative provided that all duct temperatures

indications for the cabin are operative on the COND SD

page.


GENERAL INFORMATION

Two amber crosses replace the cabin zone temperature

indications on the COND SD page.Refer to Item 21-07-03-01 Indications on the COND SD

page

The INOP SYS column on the STATUS SD page may

display the LAV DET message.

The cabin zone temperature regulation is lost.

The Air Conditioning System Controller commands FWD

and AFT cabin ducts temperature using the position of the

FWD CABIN selector and the AFT CABIN selector on the

AIR COND overhead panel.

Slight effect on cabin comfort may occur.

The cockpit temperature regulation is still operative.

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.09

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics Equipment

Ventilation

21-26-01 Avionics Blower

Fan

Note:

During ground operation, correct


21-26-01A VENT AVNCS

SYS FAULT not

displayed

C 1 0 (O) May be inoperative provided that:

1) The BLOWER pb-sw is set to OVRD,

2) Both air conditioning packs are operative, and

3) The VENT AVNCS SYS FAULT alert is notdisplayed.



- Supply the aircraft electrical network.

- Check that the air conditioning correctly operates with

both air conditioning packs set to on.

- BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD

- Check that the VENT AVNCS SYS FAULT and VENT

EXTRACT FAULT alerts are not displayed on the EWD.

· If the VENT EXTRACT FAULT alert is displayed on

the EWD, the blower fan may be seized. In that case:

- Contact the maintenance personnel to exchange the

blower fan and the extract fan.

Only the VENT EXTRACT FAULT alert must then be

displayed on the EWD.

- When the blower and extract fans are exchanged, Refer

to Item 21-26-02 Avionics Extract Fan



SEQUENCE


I T E M

01.21.10

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Fan

21-26-01B Air conditioning

inlet valve

checked open

C 1 0 (O)(M) May be inoperative provided that:



3) The air conditioning inlet valve is checked open beforeeach flight.






- BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD

- Check that the VENT EXTRACT FAULT alert is not

displayed on the EWD







- When the blower and extract fans are exchanged, Refer to Item 21-26-02 Avionics Extract Fan

MAINTENANCE PROCEDURE

Refer to AMM 21-26-00-040-006

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.11

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation


Fan

21-26-01C Avionics

ventilation

system checked



2) Both air conditioning packs are operative,

3) The air conditioning inlet valve is secured in theopen position, and

4) The avionics ventilation system is checked beforeeach flight.




- Check that air the conditioning correctly operates with


- BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD

- Check that the VENT EXTRACT FAULT alert is not

displayed on the EWD

· After application of the maintenance procedure:

Clear the VENT AVNCS SYS FAULT alert using the CLR

pb.

The VENT AVNCS SYS FAULT alert will be displayedafter landing

(Cont’d on next page)



SEQUENCE


I T E M

01.21.12

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Fan

21-26-01C Avionics

ventilation

system checked

(cont’d) OPERATING PROCEDURES (cont’d)







- When the blower and extract fans are exchanged, Refer

to Item 21-26-02 Avionics Extract Fan


Refer to AMM 21-26-00-040-013

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.13

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation

21-26-02 Avionics Extract

Fan

Note:

During ground operation, correct



SYS FAULT not

displayed


1) The blower fan is operative,

2) The EXTRACT pb-sw is set to OVRD,




FLIGHT PREPARATION/LIMITATIONS

Time limitation on ground with electrical network supplied:

OAT (°C) £ 38 £ 45 £ 55

MAX TIME No limit 3 h 35 min





- EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD

- Clear the VENT EXTRACT FAULT alert using the CLR

pb.




SEQUENCE


I T E M

01.21.14

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Fan


SYS FAULT

not displayed

(cont’d)

OPERATING PROCEDURES (Cont’d)

- AVNCS VENT/EXTC/FAN (123VU AE2) (A320)

- AVNCS VENT/EXTC/FAN (123VU AC4) (A321)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull

- Check that the VENT AVNCS SYS FAULT alert is not


Note:



C/B . . . . . . . . . . . . . . . . . . . . . . . . . Pull


engine start






inlet valve

checked open





4) The air conditioning inlet valve is checked open beforeeach flight.


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.15

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation


Fan


inlet valve

checked open

(cont’d)




OAT (°C) £ 38 £ 45 £ 55




- Check that the air conditioning correctly operates withboth air conditioning packs set to on.



pb.

- AVNCS VENT/EXTC/FAN (123VU AE2 or AC4)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull




SEQUENCE


I T E M

01.21.16

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Fan


inlet valve

checked open

OPERATING PROCEDURES (cont’d)

Note:



C/B. . . . . . . . . . . . . . . . . . . . . . . . . . Pull


engine start






Refer to AMM 21-26-00-040-007

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.17

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation


Fan

21-26-02C Avionics

ventilation

system checked










OAT (°C) £ 38 £ 45 £ 55








pb.

- AVNCS VENT/EXTC/FAN (123VU AE2 or AC4)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull




SEQUENCE


I T E M

01.21.18

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Fan

21-26-02C Avionics

ventilation

system checked

(cont’d)



Clear the VENT AVNCS SYS FAULT alert using the CLR

pb.

The VENT AVNCS SYS FAULT alert will be displayed

after landing.

Note:



C/B. . . . . . . . . . . . . . . . . . . . . . . . . . PullThe C/B must be closed again after first

engine start






Refer to AMM 21-26-00-040-015

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.19

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation

21-26-03 Avionics Skin

Exchanger Inlet

Bypass Valve

21-26-03A C 1 0 (O)(M) May be inoperative provided that:

1) The avionics skin exchanger inlet bypass valve is

manually secured in the closed position, and2) The avionics ventilation system is checked before

each flight.

Note:




ON GROUND


Clear the VENT AVNCS SYS FAULT alert displayed on

the EWD using the CLR pb.


after landing.


Refer to AMM 21-26-00-040-001



SEQUENCE


I T E M

01.21.20

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation

21-26-04 Avionics Skin Air

Outlet Valve


1) The internal flap is manually secured in the openposition,

2) The skin air outlet valve is displayed in a partially openposition amber or green on the CAB PRESS SD page,


4) The skin exchanger isolation valve is secured in theopen position, and


Note:




I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.21

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation


Outlet Valve

21-26-04A (cont’d) OPERATING PROCEDURES

ON GROUND





after landing.

· If the VENT SKIN VALVE FAULT alert is displayed

on the EWD:

Apply the ECAM procedure.

Note: Avionics smoke may be not perceptible

from the cockpit due to the opening of

the internal flap of the valve.

In the case of AVIONICS SMOKE alert:

Apply the ECAM procedure even if the

smoke is not perceptible.


Refer to AMM 21-26-00-040-002

21-26-05 Avionics Skin Air Inlet Valve

Note:






SEQUENCE


I T E M

01.21.22

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Inlet Valve (cont’d)

21-26-05A Air Conditioning

Inlet Valve open

on ground


1) The avionics skin air inlet valve is manually secured in

the closed position,2) The air conditioning inlet valve is open on ground, and





- Check that the air conditioning is operating with both air

conditioning packs set to on.


- Check that the skin air inlet valve is closed on the CAB

PRESS SD page.

- Clear the VENT AVNCS SYS FAULT alert displayed on


Note:

With only one air conditioning pack

operative, operating time on ground is

limited to 1 h.


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.23

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation


Inlet Valve

21-26-05A Air Conditioning

Inlet Valve open

on ground

(cont’d) OPERATING PROCEDURES (Cont’d)

AFTER TAKEOFF

EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

AFTER LANDING

EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . OVRD


Refer to AMM 21-26-00-040-004

21-26-05B Air Conditioning

Inlet Valve

Secured Open


1) The avionics skin air inlet valve is manually securedin the closed position,






SEQUENCE


I T E M

01.21.24

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Inlet Valve


Inlet Valve

Secured Open

(Cont’d) OPERATING PROCEDURES






- Check that the skin air inlet valve is closed on the CAB

PRESS SD page.





after landing.


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.25

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation


Inlet Valve


Inlet Valve

Secured Open


Note:

With only one air conditioning pack

operative, operating time on ground is

limited to 1 h.

AFTER TAKEOFF

EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

AFTER LANDING

EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . OVRD


Refer to AMM 21-26-00-040-014


Exchanger

Isolation Valve

Note:



21-26-06A Valve

inoperative in

the open

position

C 1 0 (O)(M) May be inoperative in the open position provided that the

avionics ventilation system is checked before each flight.




SEQUENCE


I T E M

01.21.26

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Exchanger

Isolation Valve

21-26-06A Valve

inoperative in

the open

position (cont’d) OPERATING PROCEDURES

ON GROUND




MAINTETNANCE PROCEDURE

Refer to AMM 21-26-00-040-008

21-26-06B Valve secured

open


1) The avionics skin exchanger isolation valve is securedin the open position, and

Note:

If the valve cannot be secured in the

open position, it can be interchanged

with the skin exchanger outlet bypass

valve.

2) The avionics ventilation system is checked before

each flight.


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.27

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation


Exchanger

Isolation Valve

21-26-06B Valve secured

open (Cont’d) OPERATING PROCEDURES

ON GROUND





Refer to AMM 21-26-00-040-016



SEQUENCE


I T E M

01.21.28

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation


Exchanger Outlet

Bypass Valve

21-26-07A C 1 0 May be inoperative.

Note:



21-26-08 Avionics Air

Conditioning Inlet

Valve


1) The avionics air conditioning inlet valve is manuallysecured in the open position,

2) Both air conditioning packs are operative, and3) The avionics ventilation is checked before each flight.

Note:




ON GROUND





Refer to AMM 21-26-00-040-003

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.29

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation

21-26-09 Avionics

Ventilation Filte

Note:




SYS FAULT notdisplayed

C 1 0 (O) May be inoperative (clogged) provided that:

1) The blower and extract fans are operative,










- Check that the VENT AVNCS SYS FAULT alert is not


21-26-09B Valve checked

open

C 1 0 (O)(M) May be inoperative (clogged) provided that:


2) The EXTRACT pb-sw is set to OVRD,3) Both air conditioning packs are operative, and

4) The air conditioning inlet valve is checked openbefore each flight.




SEQUENCE


I T E M

01.21.30

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation

21-26-09 Avionics

Ventilation Filte

21-26-09B Valve checked

open (cont’d)








Refer to AMM 21-26-00-040-009

21-26-09C Valve secured

open

C 1 0 (O)(M) May be inoperative (clogged) provided that:




4) The air conditioning inlet valve is secured in the openposition, and









I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.31

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation

21-26-09 Avionics

Ventilation Filte

21-26-09C Valve secured

open (cont’d) OPERATING PROCEDURES (Cont’d)





after landing.


Refer to AMM 21-26-00-040-017

21-26-10 Avionics

Equipment

VentilationComputer (AEVC)



2) The BLOWER pb-sw and the EXTRACT pb-sw areset to OVRD,

3) The air conditioning inlet valve and the skin air outletvalve are checked in the correct position beforeeach flight,

4) The extract fan is checked operative before eachflight, and

5) The skin air inlet valve is secured in the closedposition.

Note:






SEQUENCE


I T E M

01.21.32

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-26 Avionics

Equipment

Ventilation

21-26-10 Avionics

Equipment

Ventilation

Computer (AEVC)




- Check that the conditioning is operating with both air


- BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD


Note:

If the ground horn sounds:EIS/HORN/SPLY (121VU P09)

C/B. . . . . . . . . . . . . . . . . . . . . . . . . . Pull


engine start





Note:

In the case of a low pressure in the

avionics compartment ventilation ducts,

the weather radar image may not be

displayed on the ND on ground.


the EWD using the CLR pb


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.33

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Ventilation

21-26-10 Avionics

Equipment

Ventilation

Computer (AEVC)

21-26-10A (cont’d) OPERATING PROCEDURES (Cont’d)

IN FLIGHT

· In the case of an air conditioning pack failure:

- The cabin altitude may reach about 9 700 ft, and

- The CAB PR EXCESS CAB ALT alert may be displayed

on the EWD.


Refer to AMM 21-26-00-040-005

21-28 Cargo CompartmentVentilation

21-28-03 AFT Cargo

Extraction Fan

21-28-03A C 1 0 (O) May be inoperative.



Live animals must not be carried in the aft cargo

compartment.



SEQUENCE


I T E M

01.21.34

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-28 Cargo

Compartment

Ventilation

21-28-04 AFT Cargo

Isolation Valve

21-28-04A AFT ISOL

VALVE pb-sw

FAULT light

operative

C 2 0 (O) One or both may be inoperative provided that:

1) Both valves are checked closed, and

2) AFT ISOL VALVE pb-sw FAULT light is checkedoperative.




compartment.


- ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . TEST

- Check that the AFT ISOL VALVE pb-sw FAULT light

comes on

- ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . BRT or

DIM

- AFT ISOL VALVE pb-sw. . . . . . . . . . . . . . . . . . . OFF

- Check that the AFT ISOL VALVE pb-sw FAULT light

does not come on.


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.35

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-28 Cargo Compartment

Ventilation

21-28-04 AFT Cargo

Isolation Valve

21-28-04A AFT ISOL

VALVE pb-sw

FAULT light

operative


Note:

· If the AFT ISOL VALVE pb-sw FAULT light comes

on:

The AFT cargo isolation valve must be secured in the

closed position. Refer to Item 21-28-04B AFT Cargo

Isolation Valve

21-28-04B Both valves

secured closed

C 1 0 (O)(M) One or both may be inoperative provided that both valves

are secured in the closed position.




compartment.

ON GROUND

· When the AFT cargo isolation valves are secured in

the closed position:

The AFT isolation valves are displayed open green on theCOND SD page.


Refer to AMM 21-28-00-040-002



SEQUENCE


I T E M

01.21.36

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-31 Pressure Control

and Monitoring

21-31-01 Automatic Cabin

Pressure Control

System (CPC,

Outflow Valve

AUTO Channel)

21-31-01A Automatic CPC

1 inoperative

A 2 1 (O)(M) Automatic cabin pressure control system 1 may be

inoperative for three flight days provided that:

1) It is deactivated,

2) The cabin pressure indications on the CAB PRESS SDpage are checked operative in manual mode,

3) The LDG ELEV selector MAN function is operative,and

4)Extanded overwater flight is prohibited.



· If CPC 1 is affected:

AIR COND/CAB/PRESS/CTL 1 (49VU D09)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull

· If CPC 2 is affected:

AIR COND/CAB/PRESS/CTL 2 (122VU Y22)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull

- RPCU (122VU X23) C/B . . . . . . . . . . . . . . . . . . . Pull

- MODE SEL pb-sw. . . . . . . . . . . . . . . . . . . . . . . . MAN

- On the CAB PRESS SD page, check that the cabin

differential pressure, the cabin vertical speed, the cabin

altitude, and the outflow valve position are available.


I T E M

30 JUN 12MEL

A320/321MEL/CDL 01.21.37

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-31 Pressure Control and

Monitoring


Pressure Control

System (CPC,

Outflow Valve

AUTO Channel)

21-31-01A Automatic CPC

1 inoperative


- MAN V/S CTL sw . . . . . . . . . . . . . . . . . . . . . . . . DN

- On the CAB PRESS SD page, check outflow valve

movement.

- RPCU (122VU X23) C/B . . . . . . . . . . . . . . . . . . . Push

- MODE SEL pb-sw. . . . . . . . . . . . . . . . . . . . . . . . AUTO

21-31-01B Automatic CPC

2 inoperative

C 2 1 (O)(M) Automatic cabin pressure control system 2 may be

inoperative provided that:

1) It is deactivated,

2) The cabin pressure indications on the CAB PRESSSD page are checked operative in manual mode,and

3) The LDG ELEV selector MAN function is operative.


Refer to item 21-31-01A for operating procedures



SEQUENCE


I T E M

01.21.38

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


and Monitoring


Pressure Control

System (CPC,

Outflow Valve

AUTO Channel)

21-31-01C Both automatic

CPCs

inoperative

C 2 0 Both may be inoperative provided that:

1) The manual cabin pressure control system isoperative, and

2) The flight is not pressurized.

Refer to FCOM/PRO-SPO-20 Fligt Without Cabin

Pressurized.

Flight must conducted in accordance with FOPM CH 8

Maintenance Ferry Flights.

21-31-02 Manual CabinPressure Control

System (MAN V/S

CTL selector,

Outflow Valve

MAN Channel)

21-31-02A C 1 0 (M) May be inoperative provided that:

1) The LDG ELEV selector MAN function is operative,and

2) Both automatic cabin pressure control systems arechecked operative before each flight.


Refer to AMM 21-31-00-040-002

I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.39

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-31 Pressure Control and

Monitoring

21-31-03 Pressure Safety

Valve

21-31-03A C 2 1 (M) One may be inoperative in the closed position provided

that:

1) Both automatic cabin pressure control systems are

operative, and2) The three outflow valve motors are checked

operative.


Refer to AMM 21-31-00-040-001

21-31-04 Landing Elevation

Selection AUTO

Function



BEFORE TAKEOFF

- Set the LDG ELEV selector on the CABIN PRESS panel

at the destination airport altitude.

- On the CAB PRESS SD page, check that the LDG ELEV

MAN message is displayed .



SEQUENCE


I T E M

01.21.40

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


and Monitoring

21-31-05 Landing Elevation

Selection MAN

Function

21-31-05A C 1 0 (O) May be inoperative provided that:

1) The landing elevation selection AUTO function is

operative, and2) Both FMGCs are operative.



On the CAB PRESS SD page, check that the LDG ELEV

AUTO message is displayed to confirm correct position of

the LDG ELEV selector.

Note:

The landing field elevation of the

destination airport may not be correctly

displayed on the CAB PRESS SD page.

It is automatically corrected after first

engine start.

21-43 Cargo

Compartment

Heating

21-43-02 AFT Cargo

Compartment

Heating

21-43-02A HOT AIR pb-sw

OFF

C 1 0 (O) Hot air pressure regulating valve or trim air valve may be


1) The HOT AIR pb-sw on the CARGO HEAT overheadpanel is set to OFF, and

2) The operative valve is indicated closed on the CONDSD page.


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.21.41

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Heating

21-43-02 AFT Cargo

Compartment

Heating

21-43-02A HOT AIR pb-sw

OFF (cont’d)



AFT CARGO compartment heat is not be available. Live

animals and/or temperature sensitive cargo, must not be

carried in the aft cargo compartment.


- HOT AIR pb-sw (on the CARGO HEAT overhead

panel)...................................................... OFF

- On the COND SD page, check that the operative valve

(either the hot air pressure regulating valve or the trim air

valve) is indicated closed.

21-43-02B Valves secured

closed

C 1 0 (O)(M) Hot air pressure regulating valve or trim air valve may be

inoperative provided that one of these valves is secured in

the closed position.



AFT CARGO compartment heat is not be available. Live

animals and/or temperature sensitive cargo, must not be

carried in the aft cargo compartment.

MAINTENANCE PROCEDURERefer to AMM task



SEQUENCE


I T E M

01.21.42

AIR CONDITIONING

A320/321MEL/CDL

12 FEB 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-51 Pack Flow Control

21-51-02 Pack Flow

Selection


21-51-03 Pack Flow Sensor

21-51-03A C 2 1 (O) One may be inoperative.

OPERATING PROCEDURE

GENERAL INFORMATION

The hot air pressure regulating valve automatically closes.

The Flow Control Valve on the affected side operates in

pneumatic backup mode.

DURING COCKPIT PREPERATION

AIR COND HOT AIR pb-sw. . . . . . . . . . . . . . . . . . OFF

21-52 Air Cooling

System

21-52-01 Air Conditioning

Pack

21-52-01D No FL

limitation

C 2 1 (O)(M)

(FD)

One may be inoperative provided that:

1) The following alerts:

AIR PACK 1(2) REGUL FAULT AIR COND CTL 1(2)-A FAULT AIR COND CTL 1(2)-B FAULTassociated with the operative pack are not displayed

on the EWD, and

2) The affected PACK 1(2) pb-sw is set to OFF, and

3) The speedbrakes are operative, and

4) The associated pack flow control valve is secured inthe closed position.


I T E M

01 MAY 12MEL

A320/321MEL/CDL 01.21.43

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-52 Air Cooling System


Pack

21-52-01D No FL

limitation

(cont’d)



PACK FLOW pb-sw (A320) . . . . . . . . . . . . . . . . . HI

ECON FLOW pb-sw (A321) . . . . . . . . . . . . . . . . . Off

IN FLIGHT

· If BLOWER pb-sw and EXTRACT pb-sw are set to

OVRD:

- The cabin altitude may reach about 9,700 ft, and

- The CAB PR EXCESS CAB ALT alert may be displayed

on the EWD


Refer to AMM 21-51-00-040-002



SEQUENCE


I T E M

01.21.44

AIR CONDITIONING

A320/321MEL/CDL

01 MAY 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-52 Air Cooling

System


Pack

21-52-01E Limitation to

31 500 ft

C 2 1 (O)(M)

(FD)


1) The flight altitude is limited to 31 500 ft, and


AIR PACK 1(2) REGUL FAULT AIR COND CTL 1(2)-A FAULT AIR COND CTL 1(2)-B FAULTassociated with the operative pack are not displayedon the EWD, and

3) The affected PACK 1(2) pb-sw is set to OFF, and

4) The associated pack flow control valve is secured inthe closed position.


Refer to Item 21-52-01D


Refer to AMM 21-51-00-040-002

I T E M

01 MAY 12MEL

A320/321MEL/CDL 01.21.45

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING



Pack

21-52-01G Air cycle

machine failed

C 2 1 (O)(FD) One may be operated on heat exchanger cooling only (air

cycle machine failure) provided that:


AIR COND CTL 1(2)-A FAULT

AIR COND CTL 1(2)-B FAULTassociated with the operative pack are not displayedon the EWD, and

2) The affected pack outlet temperature indication isoperative on the BLEED SD page.



PACK 1(2) pb-sw in "heat exchanger

cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

IN FLIGHT

· When the TAT is equal to or less than 12° C:


cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On

· If the non affected air conditioning pack fails:

Maximum flight altitude . . . . . . . . . . . . . . . . . . . . .31,500 ft


I T E M



SEQUENCE


01.21.46

AIR CONDITIONING

A320/321MEL/CDL

01 MAY 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-52 Air Cooling

System


Pack (cont’d)

21-52-01G Air cycle

machine failed


DURING DESCENT

· If the TAT is above 12° C:


cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AT THE END OF THE DESCENT, BEFORE LANDING

PACK 1(2) pb-sw in "heat exchanger cooling

only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

21-52-01H Non

pressurizedflight

C 2 0 Both may be inoperative provided that the flight is not

pressurized.


Pressurized.

Refer to FOPM CH 8 Maintenance Ferry Flights


Pack Ram Air Inlet

Flap

21-52-02A Flap

deactivated

C 2 0 (M) One or both may be inoperative provided that the affected

flap is deactivated in the open position.


Refer to AMM 21-61-00-040-002

21-52-02B Only one

inoperative

C 2 1 One may be inoperative in the closed position provided

that the associated air conditioning pack is considered

inoperative.

Refer to Item 21-52-01 Air Conditioning Pack

I T E M

01 MAY 12MEL

A320/321MEL/CDL 01.21.47

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING



Pack Ram Air Inlet

Flap

21-52-02C Non

pressurized

flight

C 2 0 Both may be inoperative in the closed position provided

that the flight is not pressurized.

Refer to FCOM/PRO-SPO-20 Fligt Without CabinPressurized.


21-55 Emergency Ram Air

Inlet

21-55-01 Emergency Ram

Air Inlet

21-55-01A Ram air inlet

deactivated

C 1 0 (M) May be inoperative provided:

1) The emergency ram air inlet is deactivated in theclosed position, and

2) Both air conditioning packs are checked operative.


Refer to AMM 21-55-00-040-002

21-55-01B Non

pressurized

flight

C 1 0 May be inoperative in the open position provided that:

1) Extended overwater flight is not conducted, and



Pressurized.


I T E M



SEQUENCE


01.21.48

AIR CONDITIONING

A320/321MEL/CDL

01 MAY 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONIN

21-61 Pack Temperature

Control

21-61-01 Pack Turbine

Bypass Valve


21-63 Cockpit and Cabin

Temperature

Control

21-63-02 Cockpit and Cabin

Trim Air Valve

21-63-02A Affected valve

checked closed

C 3 0 (O) One or more may be inoperative provided that the

affected valve is checked closed on the COND SD page.



On the COND SD page page, check that the affected trim

air valve is closed amber.

IN FLIGHT

· If the affected zone temperature becomes

uncomfortable:

HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

21-63-02B Hot air pressure

valve checked

operative

C 3 0 (O) One or more may be inoperative provided that the hot air

pressure regulating valve is checked operative on the

COND SD page.


I T E M

01 MAY 12MEL

A320/321MEL/CDL 01.21.49

AIR CONDITIONING



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONIN


Temperature Control

21-63-02 Cockpit and Cabin

Trim Air Valve

21-63-02B Hot air pressure

valve checked

operative

(cont’d)



- HOT AIR pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . OFFthen on

- On the COND SD page, check that the hot air pressure

regulating valve follows the HOT AIR pb-sw command.

IN FLIGHT

· If affected zone temperature becomes

uncomfortable:

HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

21-63-02E Hot air pressurevalve

considered

inoperative

C 3 0 One or more may be inoperative provided that the hot air pressure regulating valve is considered inoperative.

Refer to Item 21-63-03 Hot Air Pressure Regulating Valve

21-63-03 Hot Air Pressure

Regulating Valve

21-63-03A Hot air pressure

valve checked

closed

C 1 0 (O) May be inoperative in the closed position provided that:

1) HOT AIR pb-sw is set to OFF, and

2) Hot Air Pressure Regulating Valve is checked closedon the COND SD page.


I T E M



SEQUENCE


01.21.50

AIR CONDITIONING

A320/321MEL/CDL

01 MAY 12MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONIN


Temperature

Control


Regulating Valve

21-63-03A Hot air pressure

valve checked

closed (cont’d)



- HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF

- On the COND SD page page, check that the hot air

pressure regulating valve is closed amber.

21-63-03B All trim valve

checked closed

C 1 0 (O) May be inoperative in the open position provided that:

1) HOT AIR pb-sw is set to OFF, and

2) All Trim Air Valves are checked closed on the CONDSD page.


GENERAL INFORMATION

On the COND SD page, the hot air pressure regulating

valve is displayed amber open.


- HOT AIR pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . OFF

- On the COND SD page, check that all the trim air valves

are closed amber.

21-63-03C Hot air pressure

valve secured

closed

C 1 0 (O)(M) May be inoperative provided that the hot air pressure

regulating valve is secured in the closed position.


01 MAY 12MEL

A320/321MEL/CDL 01.21.51

AIR CONDITIONING



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING


Temperature Control


Regulating Valve

21-63-03C Hot air pressure

valve secured

closed (cont’d) OPERATING PROCEDURES

GENERAL INFORMATION

On the COND SD page, the hot air pressure regulating

valve is displayed closed amber.


Refer to AMM 21-63-00-040-002


System Controller

Channel (COND

CTL 1(2)-A(B))

21-63-04A C 4 2 One may be inoperative on each side.

* * *



SEQUENCE


01.21.52

AIR CONDITIONING

A320/321MEL/CDL

01 MAY 12MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-01 FLT CTL

Overhead Panel

22-01-01 FAC pb-sw

FAULT light


22-01-02 FAC pb-sw OFF

light

22-01-02A C 2 0 One or both may be inoperative.

22-05 FMA Indications

on the PFD

22-05-01 AP Related

Indications on

the FMA

22-05-01A B 2 1 One or more indications may be inoperative on one

FMA.

22-05-01B B 2 0 (O) One or more indications may be inoperative on both

FMAs provided that that AP is not used.



RVSM operations are not permitted.

Maximum landing capability is CAT I.

22-05-02 A/THR Related

Indications on

the FMA

22-05-02A B 2 1 One or more indications may be inoperative on one

FMA.

22-05-02B B 2 0 One or more indications may be inoperative on both

FMAs provided that the autothrust (A/THR) is considered

inoperative.

Refer to Item 22-30-01 Autothrust (A/THR)

12 FEB 12MEL

A320/321MEL/CDL 01.22.01

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-05 FMA Indications on

the PFD

22-05-03 Approach and

Landing

Capabilities on

the FMA

22-05-03A C 2 0 (O) One or more may be inoperative on one or both FMAs.




22-05-04 Special

Messages on the

FMA

22-05-04A B 2 1 “MAN PITCH TRIM ONLY” is required on one side.

22-10 Autopilot/Flight

Director (AP/FD)

22-10-01 Autopilot (AP)

22-10-01A B 2 1 (O) One may be inoperative.



- When one AP is inoperative:

Landing capability is CAT II.




SEQUENCE


I T E M

01.22.02

AUTO FLIGHT


MEL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT


Director (AP/FD)

22-10-01 Autopilot

(AP)(Cont’d)

22-10-01B A 2 0 (O)(FD) Both may be inoperative provided:

1) Current weather enroute does not indicatethrunderstorm, activites, and approach minimums

are limited to CAT I or higher,2) Aircraft is not dispatched into RVSM airspace,

3) For international flight Aircraft is released for one legfly ( 2 ½ hours maximum) to a maintenance stationfor repair,

4) For domestic flight Aircraft is released for two leg fly( 2 hours total ) to a maintenance station for repair,


- When both APs are inoperative:

RVSM operations are not permitted.Maximum landing capability is CAT I.

22-10-02 Flight Director

(FD)

22-10-02A B 2 1 (O)(FD) One may be inoperative.


FOR TAKEOFF

- For a takeoff without one FD:

Refer to FCOM /PRO No Flight Director Takeoff

22-10-03 Take-over pbPriority Function

22-10-03A 2 2 Both must be operative.

12 FEB 12MEL

A320/321MEL/CDL 01.22.03

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT


Director (AP/FD)

22-10-04 Take-over pb AP

Disconnection

Function

22-10-04A B 2 1 (O)(FD) One may be inoperative.




BEFORE ENGINE START

- AP 1 · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Operative take-over pb · · · · · · · · · · · · · · · · · · · · Press

- Check that the red AP OFF message is displayed onthe EWD.

- AP 2 · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Operative take-over pb · · · · · · · · · · · · · · · · · · · · Press

- Check that the red AP OFF message is displayed onthe EWD.

BEFORE APPROACH

- If the AP is used for approach:

The operative AP disconnect pb must be assigned tothe PF.



SEQUENCE


01.22.04

AUTO FLIGHT


MEL

I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT


Director (AP/FD)

22-10-05 AUTO LAND

lights

22-10-05A C 2 0 (O)(FD) One or both may be inoperative.



- If Captain side or both lights are inoperative:


22-10-06 AP

Disengagement

Warning

22-10-06A C 1 0 (O)(FD) May be inoperative provided that the AP is not engaged.





22-10-07 Sticks and

Rudder Pedals

Locking

Solenoid in AP

Mode

22-10-07A C 3 1 (O)(FD) One or two may be inoperative unlocked provided that

no autoland is performed.




01 MAY 12MEL

A320/321MEL/CDL 01.22.05

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-30 Autothrust

22-30-01 Autothrust

(A/THR)

22-30-01A B 1 0 (O)(FD) May be inoperative provided that the autothrust (A/THR)

is disconnected before each flight.



Maximum Landing capability is CAT I.

AFTER ENGINE START

- Press and hold either autothrust instinctive disconnectpb for at least 15 seconds.

- The A/THR system is permanently disconnected for the entire flight.

Check that A/THR INOP SYS is displayed on theSTATUS SD page.

- All A/THR functions including ALPHA FLOORprotection are lost.

22-30-02 Autothrust

Instinctive

Disconnect pb

22-30-02A C 2 1 (O) One may be inoperative provided that the ability to

disconnect the autothrust (A/THR) via the remaining

Instinctive Disconnect pb and by the FCU A/THR pb is

checked before each flight.


The purpose of the procedure is to check the A/THRdisconnection via the remaining Instinctive Disconnect

pb and via the A/THR pb on the FCU.




SEQUENCE


01.22.06

AUTO FLIGHT


MEL

I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-30 Autothrust

22-30-02 Autothrust

Instinctive

Disconnect pb

22-30-02A (Cont’d) OPERATING PROCEDURES(Cont’d)

AFTER IRS ALIGNMENT

Note:

Disregard alerts during the test. Use the

EMER CANCEL pb on the ECAM

control panel as necessary.

Aircraft configuration for the check via the FMS 1:

- ENG/FADEC GND PWR 1 and 2· · · · · · · · · · · · · ON

- Both thrust levers· · · · · · · · · · · · · · · · · · · · · · · · MCT

- FD· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Off

- AUTO FLT/FMGC/2 (121 VU M17) C/B · · · · · · · Pull

- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Check that green SPEED and white A/THRindications appear on the PFD.

- Check that A/THR pb light bars are ON.

Check of the A/THR disconnection via the remaining

Instinctive Disconnect pb:

- A/THR instinctive disconnect pb (non affectedautothrust) · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push

- Check that the A/THR pb light bars are OFF.

- Check that green SPEED and white A/THR

indications are no more displayed on the PFD.


12 FEB 12MEL

A320/321MEL/CDL 01.22.07

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-30 Autothrust

22-30-02 Autothrust

Instinctive

Disconnect pb


- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Check that the A/THR pb light bars are ON.

- Check that green SPEED and white A/THR indicationsare displayed on the PFD.

Check of the A/THR disconnection via the A/THR pb on

the FCU:

- A/THR pb (on the FCU) · · · · · · · · · · · · · · · · · · · · · · Off


- Check that green SPEED and white A/THR indicationsare no more displayed on the PFD.

- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

Aircraft configuration for the check via the FMS 2:

- AUTO FLT/FMGC/2 (121VU M17) C/B · · · · · · · · Push

- AUTO FLT/FMGC/1 (49VU B02) C/B · · · · · · · · · · · Pull

- Wait 2 min.

Check of the A/THR disconnection via the remaining

Instinctive Disconnect pb:

- A/THR instinctive disconnect pb (non affectedautothrust)· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push


- Check that green SPEED and white A/THR indicationsare no more displayed on the PFD.

- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Check that the A/THR pb light bars are ON.

- Check that green SPEED and white A/THR indicationsare displayed on the PFD.




SEQUENCE


01.22.08

AUTO FLIGHT


MEL

I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-30 Autothrust

22-30-02 Autothrust

Instinctive

Disconnect pb


Check of the A/THR disconnection via the A/THR pb on

the FCU:

- A/THR pb (on the FCU) · · · · · · · · · · · · · · · · · · · · Off


- Check that green SPEED and white A/THRindications are no more displayed on the PFD.

- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

Restore normal aircraft configuration:

- A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Off

- AUTO FLT/FMGC/1 (49VU B02) C/B · · · · · · · · Push

- ENG/FADEC GND PWR 1 and 2 · · · · · · · · · · · · · Off

- Both thrust levers· · · · · · · · · · · · · · · · · · · · · · · · IDLE

- RCL pb (on the ECAM control panel) · · · · · · · · Push

- Wait 2 min before using the MCDU and the FD.

22-30-03 Autothrust

Disengagement

Warning

22-30-03A B 1 0 May be inoperative provided that the autothrust (A/THR)

is considered inoperative.


12 FEB 12MEL

A320/321MEL/CDL 01.22.09

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-60 Flight Augmentation

(FAC)

22-60-01 FAC 1

22-60-01A 1 1 (M) Must be operative.

Note:

The AUTO FLT FAC 1 FAULT alert may

be displayed with the associated AUTOFLT/FAC1/28VDC C/B tripped.

This may be due to a short circuit within

either rudder trim actuator channel 1 or

rudder travel actuator channel 1.

In this case, the FAC 1 may be

recovered provided that the affected

part of the faulty actuator is deactivated

using the associated maintenance

procedure.

Refer to AMM 27-22-00-040-001, or

Refer to AMM 27-23-00-040-01.

Refer to Item 27-22-01 Rudder Trim

System, or

Refer to Item 27-23-01 Rudder Travel

Limiter System (Including Rudder and

Pedals Travel Limiter Units)


Refer to AMM task.



SEQUENCE


01.22.10

AUTO FLIGHT


MEL

I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-60 Flight

Augmentation

(FAC)

22-60-02 FAC 2

22-60-02A C 1 0 (O)(FD) May be inoperative provided that:

1) All ADIRSs, ELACs, SECs, SFCCs, LGCIUs andRAs are operative, and

2) The Rudder Travel Limiter System 2 is consideredinoperative.

Refer to item 22-60-04 Yaw Damper System, and

Refer to item 27-22-01 Rudder Trim System, and

Refer to Item 27-23-01 Rudder Travel Limiter System

(Including Rudder and Pedals Travel Limiter Units)




ON GROUND

- If the AUTO FLT FAC 2 FAULT alert is displayedon the EWD

Or

- If erroneous speeds are displayed:

- AUTO FLT/FAC 2/28VDC (121VU M19) C/B

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull

- FAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . OFF

12 FEB 12MEL

A320/321MEL/CDL 01.22.11

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-60 Flight Augmentation

(FAC)

22-60-03 Windshear

Detection

System

Predictive

22-60-03A C 1 0 (O) May be inoperative provided:

1)Alternate procedures are established and used,and

2)GPWS windshear alert mode (Mode 7) is operative.


Flight Crewmember must refer to the winshear section,

in the FCOM . prior to their first departure of the day.

22-60-03B A 1 0 (O)(FD) May be inoperativeprovided:

1)alternate procedures are estalished and used

2)Takeoff and landings are not condcuted in known or forecast windshear conditions, and

3)Repairs are made within three flight days.


Flight Crewmember must refer to the winshear section,

in the FCOM prior to their first departure of the day.



SEQUENCE


01.22.12

AUTO FLIGHT


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-60 Flight

Augmentation

(FAC)

22-60-04 Yaw Damper

System

22-60-04A C 2 1 (O)(M)

(FD)

One may be inoperative.





Refer to AMM 27-26-00-040-001

22-70 Flight

Management

System (FMS)

22-70-01 Flight

Management

System (FMS)

22-70-01A FMS 1

inoperative with

IR 1 (NAV

mode) or GPS

1 operative

C 2 1 (O) The FMS 1 may be inoperative provided that:

1) Two MCDUs are operative, and

2) The IR 1 NAV mode or GPS 1 is operative.


IN FLIGHT

- In the case of FMS 1+2 failure:

MCDU NAV B/UP · · · · · · · · · · · · · · · · · · · · · · · · UseRefer to FCOM/DSC-22-20-60-130 (MCDU BACKUP NAVIGATION).

12 FEB 12MEL

A320/321MEL/CDL 01.22.13

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-70 Flight Management

System (FMS)

22-70-01B FMS 2

inoperative

with IR 1

(NAV mode)

or GPS 1

operative

C 2 1 (O) The FMS 2 may be inoperative provided that the IR 1

NAV mode or GPS 1is operative.


Refer to MEL 22-70-01A

22-70-01C FMS 1

inoperative

C 2 1 The FMS1 may be inoperative provided that the flight

remains within radio navaids coverage.

22-70-02 NavigationDatabase

22-70-02A C 2 0 (O)(FD) May be out of currency provided:

1)Current Aeronautical Charts are used to verifyNavigation Fixes before dispatch, and

2)Procedures are established and used to verify statusand suitability of Navigation Facilties used to defineroute of flight.




SEQUENCE


01.22.14

AUTO FLIGHT


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-70 Flight

Management

System (FMS)

22-70-02 Navigation

Database


1. Both, pilots and dispatch must check the flight plan

route against current aerounautical cfhart(s) andNOTAMs for suitability and serviceability of NAVFixes.

2. Pilot must ensure that all applicable charts for enroute to destination and alternate(s) are availableon board.

3. All required terminal and approach plates areavailable on board, and

4. Cross check FMGS waypoints using current flighcrew navigation charts.

22-70-03 Performance

Information


22-70-04 Fuel/Time

Prediction


12 FEB 12MEL

A320/321MEL/CDL 01.22.15

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-81 Flight Control Unit

(FCU)

22-81-01 Auto Flight

Control Panel

(FCU)

22-81-01-01 AP Engagement

pb

22-81-01-01A B 2 1 One may be inoperative provided that the associated

autopilot (AP) is considered inoperative.

Refer to Item 22-10-01A Autopilot (AP)

22-81-01-01B A 2 0 Both may be inoperative provided that both autopilots

(AP) is considered inoperative.

Refer to Item 22-10-01B Autopilot (AP)

22-81-01-02 A/THR Arming

pb

22-81-01-02A B 1 0 May be inoperative provided that the autothrust (A/THR)is considered inoperative.


22-81-01-03 Mode

Engagement pb

(LOC, EXPED,

APPR)

22-81-01-03A B 3 0 One or more may be inoperative.

22-81-01-04 Selection knob

(ALT, HDG-TRK,SPD-MACH)

22-81-01-04A 3 3 Must be operative.



SEQUENCE


01.22.16

AUTO FLIGHT


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT


(FCU)

22-81-01 Auto Flight

Control Panel

(FCU)

22-81-01-05 V/S-FPA

Selection knob

22-81-01-05A B 1 0 May be inoperative provided that operations do not

required its use.

22-81-01-06 HDG-V/S/TRK-

FPA Change

Over pb

22-81-01-06A B 1 0 May be inoperative provided that the HDG-V/S selection

is operative.

22-81-01-07 SPD/MACH

Change Over pb

22-81-01-07A C 1 0 May be inoperative provided that the SPD selection is

operative.

22-81-01-08 METRIC ALT pb


22-81-01-09 Selection

Window (SPD-

MACH, HDG-

TRK, ALT, V/S-

FPA)

22-81-01-09B C 4 0 One or more may be inoperative provided that the

associated indications are operative on both PFDs and

both Nds.

12 FEB 12MEL

A320/321MEL/CDL 01.22.17

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT


(FCU)

22-81-02 EFIS Control

Panel (FCU)

22-81-01-10 AP1, AP2 and

A/THR pb light

Bars

22-81-01-10A C 3 0 One or more may be inoperative provided that the

associated indication is operative on both PFDs.

22-81-01-11 Mode

Engagement

(LOC, EXPED,

APPR) pb light

Bars

22-81-01-11A C 3 0 One or more may be inoperative.

22-81-02-01 Baro Reference

Display Window

22-81-02-01A C 2 1 One may be inoperative.


selector Outer

Ring (in Hg/hPa)

22-81-02-02A C 2 1 One may be inoperative provided that the unit required

for the intended flight is operative on both EFIS control

panels.


selector Inner knob

22-81-02-03A 2 2 Both must be operative.



SEQUENCE


01.22.18

AUTO FLIGHT


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT


(FCU)


Panel (FCU)

22-81-02-04 FD pb

22-81-02-04A B 2 1 One may be inoperative provided that the associated FD


Refer to Item 22-10-02 Flight Director (FD)

22-81-02-05 LS pb

22-81-02-05A C 2 1 One may be inoperative provided that the associated ILS


Refer to Item 34-30-04 Instrument Landing System (ILS)

22-81-02-06 Optional Data

(ARPT, NDB,

VOR.D, WPT,

CSTR) Displaypb


22-81-02-07 ND Range

selector

22-81-02-07A B 2 1 One may be inoperative provided that the ND unit

associated with the operative ND range selector is

operative.

22-81-02-08 ND Mode

selector

22-81-02-08A B 2 1 One may be inoperative provided that the ND unit

associated with the operative ND mode selector is

operative.

12 FEB 12MEL

A320/321MEL/CDL 01.22.19

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT


(FCU)


Panel (FCU)

22-81-02-09 ADF/VOR sw


associated ADF/VOR indication on ND is consideredinoperative.

Refer to Item 34-50-03A ( ADF )

Refer to Item 34-50-05A ( VOR )

Refer to Item 34-06-06 Radio Navaids Indications on the

ND

22-81-02-10 LS and FD pb

light Bars

22-81-02-10A C 4 2 One per each side may be inoperative provided that the

associated indication is displayed on both PFDs.

22-81-02-11 Optional Data

(ARPT, NDB,

VOR.D, WPT,

CSTR) Display

pb light Bars


22-81-03 FCU Channel

22-81-03-01 FCU Channel

22-81-03-01A C 2 1 One channel may be inoperative provided that Two

RMPs, all DUs, both RAs, both LGCIUs, both FACs,

both Automatic Cabin Pressure Control Systems, all

ADIRUs and the ISIS Baro-altimeter function are

operative.



SEQUENCE


01.22.20

AUTO FLIGHT


MEL

I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-82 Multipurpose

Control and

Display Unit

(MCDU)

22-82-01 MCDU 1

22-82-01B B 1 0 May be inoperative provided that:

1) The MCDU 2 is operative, and

2) The flight remains within radio navaids coverage.

22-82-02 MCDU 2

22-82-02B Flight within

navaids

coverage

B 1 0 May be inoperative provided that the flight remains

within radio navaids coverage.

22-82-04 MCDUAnnunciator

light

22-82-04A C 8 0 One or more may be inoperative.

12 FEB 12MEL

A320/321MEL/CDL 01.22.21

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-83 Flight Management

and Guidance

Computer (FMGC)

22-83-01 Flight

Management

and Guidance

Computer

(FMGC)

22-83-01A FMGC 1

inoperative

A 2 1 (O) One may be inoperative for three flight days provided

that:

1)FMGC 1 is deactivated,

2) FMS 1 is considered inoperative,

Refer to Item 22-70-01 Flight Management System(FMS), and

3)The terrain function of TAWS is consideredinoperative.

Refer to Item 34-40-01 Ground Proximity Warning

System (GPWS)/Terrain Awareness and Warning

System (TAWS)





- If FMGC 1 is affected:

AUTO FLT/FMGC/1 (49VU B02 or 121VU M16) C/B· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull

- If ADS-B is required for the intended flight:

ATC selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

- If FMGC 2 is affected:

AUTO FLT/FMGC/2 (121VU M17) C/B· · · · · · · · · · Pull




SEQUENCE


01.22.22

AUTO FLIGHT


MEL

I T E M

7/23/2019 A 320321 Mel Cdl


22 AUTO FLIGHT

22-83 Flight

Management and

Guidance

Computer (FMGC)

22-83-01 Flight

Management

and Guidance

Computer

(FMGC)

22-83-01A FMGC 1

inoperative

(Cont’d)


Note:

During IR alignment, when the FMGC 2

is deactivated, IRS IN ALIGN memo

cannot be displayed until the FD 1 is

engaged.

- If ADS-B is required for the intended flight: ATC selector · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · 1

22-83-01B FMGC 2

inoperative

C 2 1 (O) FMGC 2 may be inoperative provided that:

1) FMGC 2 is deactivated, and

2) FMS 2 is considered inoperative.

Refer to Item 22-70-01 Flight Management System

(FMS)


Refer to MEL 22-83-01A for operating procedure.

* * *

12 FEB 12MEL

A320/321MEL/CDL 01.22.23

AUTO FLIGHT



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl





SEQUENCE


01.22.24

AUTO FLIGHT

A320/321MEL/CDL

MEL

I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-00 MAINTENANCE

Message on the

STATUS SD page

23-00-01 CIDS 1(2)

MAINTENANCE

Message

23-00-01A C 1 - CIDS 1(2) MAINTENANCE message may be displayed on

the STATUS SD page.


23-01-01 RCDR Overhead

Panel

22-01-01-01 RCDR GND CTL

pb-sw ON light


22-01-01-31 RCDR GND CTL

pb-sw

22-01-01-31A AUTO Position C 1 0 (O) May be inoperative in the AUTO position.


ON GROUND

CVR can only be tested through the CVR test pb-sw

during the first 5 minutes after supply of the aircraft

electrical network.

22-01-01-31B ON Position C 1 0 (O) May be inoperative in the ON position.


AFTER LANDING

- To stop CVR recording, if needed:

COM/CVR/SPLY (49 VU E14) C/B · · · · · · · · · · · PULL

22-01-01-31C CVR

Considered

Inoperative

A 1 0 May be inoperative provided that the CVR is considered

inoperative.

Refer to Item 23-71-01 Cockpit Voice Recorder (CVR)

12 FEB 12MEL

A320/321MEL/CDL 01.23.01

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS


23-01-01 RCDR Overhead

Panel

23-01-01-32 CVR ERASE pb


23-01-01-33 CVR TEST pb

23-01-01-33A A 1 0 May be inoperative provided that the Cockpit Voice

Recorder (CVR) is considered inoperative.

Refer to Item 23-71-01 Cockpit Voice Recorder (CVR)

23-01-02 CALLS Overhead

Panel

23-01-02-31 CALLS ALL pb


23-01-02-32 CALLS EMER pb

CALLS FWD pb,

CALLS MID pb,

CALLS EXIT pb,

CALLS AFT pb

23-01-02-32A Use of

Passenger

address system

C 1 0 (O) May be inoperative provided that the passenger address

system is used for communication between the cockpit

and the cabin.


PIC will brief cabin crew that he will use passenger

address system for communications.



SEQUENCE


I T E M

01.23.02COMMUNICATIONS


MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS


23-01-02 CALLS

Overhead Panel

23-01-02-32 CALLS EMER pb

CALLS FWD pb,

CALLS MID pb,

CALLS EXIT pb,

CALLS AFT pb

23-01-02-32B Use of Cockpit

handset

interphone

C 1 0 (O) May be inoperative provided that the cockpit handset

interphone is used for communication between the cockpit

and the cabin.


PIC will brief cabin crew that he will use cockpit handset

interphone for communications.

12 FEB 12MEL

A320/321MEL/CDL 01.23.03

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-09 ECAM Alerts

23-09-01 COM HF 1(2)

EMITTING Alert

23-09-01A Refer to Item 23-10-01 HF System

23-09-02 COM VHF 1(2)(3)

EMITTING Alert

23-09-02A C 3 2 (O) One may be displayed provided that :

1) The alert is confirmed to be false by troubleshooting,and

2) The affected VHF is deactivated and consideredinoperative.

Refer to Item 23-10-02 VHF System


GENERAL INFORMATION

To make troubleshooting easier, Refer to FCOM/PRO- ABN-23 COM VHF 1(2)(3)/HF 1(2) EMITTING.


· To deactivate the VHF1 system, apply:

COM/VHF/1 (49 VU G09) C/B . . . . . . . . . . . . . . . . PULL


COM NAV/VHF/2 (121 VU L04) C/B . . . . . . . . . . . PULL


COM NAV/VHF/3 (121 VU L05) C/B . . . . . . . . . . . PULL



SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-10 Speech

Communication

23-10-01 HF System

23-10-01A 1 1 (FD) Must be operative on routes that require HF

communication with ATSU, provided SATCOM Voice

Mode is available for use by that unit.

C 1 0 (FD) May be inoperative provided SATCOM Voice Mode isoperative.

23-10-02 VHF System

23-10-02B C 3 2 VHF 2 or VHF 3 may be inoperative.

Note:

The VHF 3 may be used as one of the

VHFs required by regulations, provided

that the VHF 3 is set to VOICE mode

before each flight.

23-10-03 SATCOM Voice

Mode

23-10-03A 1 1 (FD) Must be operative on routes that require HF

communication with ATSU.

C 1 0 (FD) May be inoperative provided HF System and SELCAL

Function are operative.

23-13 Radio Management

23-13-01 RadioManagement

Panel (RMP)

23-13-01B C 3 2 RMP 2 may be inoperative.

01 MAY 12MEL

A320/321MEL/CDL 01.23.05

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-13 Radio Management

23-13-02 RMP Selection Key

23-13-02A C 3 2 One may be inoperative on each RMP provided that :

1) VHF 1 selection key is operative on RMP 1, and

2) If HF is required, HF 1 selection key is operative onRMP 1.

23-20 Data Transmissionand Automatic Calling

23-20-01 Aircraft

Communications

Addressing

Reporting System

(ACARS)

23-20-01A B 1 0 (O)(FD) May be inoperative provided altenate procedures are

used.


1. Flight crew must transmit depature, enroute, and thearrival reports in accordance with the route manualcommunication requirement.

2. Flight crew must complete the in-flight cruiseperformance data records if required.

NOTE:

Any portion of the system that is

operative may be used.

23-20-02 SATCOM Data

Mode

23-20-02A B 1 0 May be inoperativeprovided operation or procedures do

not requier its use.



SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-31 Passenger Address

System

23-31-01 Passenger

Address System

23-31-01A 1 1 Must be operative.

Note:

i. In the case of partial failure of thepassenger address system, refer to

the item(s) of the affected system(s).

ii. Total failure of the passenger

address system (indicated by the

COM CIDS 1+2 FAULT alert

displayed on the EWD) is not

permitted.

23-40 Interphone

23-40-01 Ground External

Horn



ON GROUND

- When the aircraft electrical network is supplied:

Monitor the avionics equipment ventilation in thecockpit.

BEFORE LEAVING THE AIRCRAFT

Set the three ADIRS Mode selectors to OFF.

23-40-02 Flight Crew

Interphone

System

23-40-02A 1 1 Must be operative for each person on cockpit duty.

12 FEB 12MEL

A320/321MEL/CDL 01.23.07

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-40 Interphone

23-40-03 Flight Crew to

Ground

Communication

System



Instruct ground crew to connect to flight interphone jack

and establish communications through flight interphone.

23-40-04 Service Interphone

Jack

23-40-04A C 8 0 (O) One or more may be inoperative.


Instruct ground crew to connect to flight interphone jack

and establish communications through flight interphone.

23-51 Audio Management

23-51-01 SELCAL Function

23-51-01A 1 1 (FD) Must be operative for dispatch from Kingdom on routes

that require HF communication with ATSU and SATCOM

Voice Mode must be operative.

C 1 0 (FD) May be inoperative for dispatch back to Kingdom on

routes that require HF communication with ATSU

provided:

1) Crew continuously monitors HF communication, and

2) SATCOM Voice Mode is operative.

C 1 0 (FD) May be inoperative provided SATCOM Voice Mode is

operative.



SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-51 Audio Management

23-51-02 Boomset

23-51-02A A 2 0 May be inoperative provided:

1) Flight data recorder and hand mic are operative, and

2) Repaire are made within three flight days.

23-51-03 Hand

Microphone

23-51-03A C 2 1 One may be inoperative provided both associated boom

micrphones are operative.

23-51-04 Cockpit

Loudspeaker

23-51-04A C 2 1 Only F/O loudspeaker may be inoperative provided that at

least one crewmember on cockpit duty wears a boomset

compatible with the quick donning oxygen mask.

23-51-05 CockpitLoudspeaker

Volume Control

23-51-05A C 2 1 (O) Only F/O side may be inoperative provided that the

affected crewmember on cockpit duty wears a boomset

compatible with the quick donning oxygen mask.


Cockpit crew will be aware and prepared for monitoring

communications during the flight.

12 FEB 12MEL

A320/321MEL/CDL 01.23.09

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-51-06 Sidestick PTT sw

23-51-06B C 2 1 (M) Only F/O side may be inoperative in the open position (non

transmitting position) provided that the INT/RAD sw on

CAPT ACP, on F/O ACP and on ACP 3 are operative.

Note:

Apply the maintenance procedure only

when the operative sidestick radio

selector is failed in the closed position(transmitting position).


Refer to AMM 23-51-00-040-001

23-52 Audio Control Panel

(ACP)

23-52-01 CAPT and F/O

ACP

23-52-01A C 2 1 (O) One may be inoperative provided that :1) ACP 3 is operative, and

2) The AUDIO SWITCHING selector is operative.


In order to recover audio channel on the affected side :

AUDIO SWITCHING.................................CAPT 3 (F/O 3)

23-52-02 ACP 3




SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-52 Audio Control Panel

(ACP)

23-52-03 Fourth Occupant

ACP


23-52-04 ACP in the

Avionics

Compartment

23-52-04A D 1 0 May be inoperative.

23-52-05 ACP

Transmission

Key

23-52-05A C 14 12 One may be inoperative on each ACP provided that :

1) VHF 1 transmission key is operative either on CAPT ACP or on F/O ACP, and

2) If HF is required, HF 1 transmission key is operativeeither on CAPT ACP or on F/O ACP.

23-52-06 ACP Reception

knob

23-52-06A C 16 14 One may be inoperative on each ACP provided that :

1) VHF 1 reception knob is operative either on CAPT ACP or on F/O ACP, and

2) If HF is required, HF 1 reception knob is operativeeither on CAPT ACP or on F/O ACP,and

3) If ILS is required for approach, one ILS reception knob

is operative either on CAPT ACP or on F/O ACP.

23-52-07 ACP Reception

knob light


12 FEB 12MEL

A320/321MEL/CDL 01.23.11

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-53 AUDIO SWITCHING

Panel on the Center

Pedestal

23-53-01 AUDIO

SWITCHING

selector


23-71 Cockpit Voice

Recorder (CVR)

23-71-01 Cockpit Voice

Recorder (CVR)


1) Flight Data Recorder (FDR) is operative, and

2) Repair is made within three flight days.

23-72 Cockpit Door

Surveillance System(CDSS)

23-72-01 Cockpit Door

Surveillance

System (CDSS)

23-72-01A C 1 0 (O)(FD) May be inoperative provided:

1) An alternate means of viewing the area on the cabinside of the flight crew compartment is available andfunctions,

2) Alternate procedures are established and used of ensuring the security of the area outside the fligh crewcompartment door,

3) With the forward camera inoperative, the cabin area infront of the cockpit must be illuminated when the cabinis in darkness, and

4) With the forward camera inoperative, an additionalcrew member must be assigned for duty in the cockpit.




SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-72 Cockpit Door

Surveillance System

(CDSS)

23-72-01 Cockpit Door

Surveillance

System (CDSS)

23-72-01A (Cont’d) OPERATING PROCEDURES

1. When the forward camera which provides a view of thearea directly in front of the cockpit is inoperative(camera 1), an additional crew member must beassigned for duty in the cockpit.

2. Before the cockpit door is opened, he/she must lookthrough the door viewing lens, identify the personseeking admission and confirm with the PIC TO OPENTHE DOOR.

3. Ensure that the cabin ceiling light of the area in front of the cockpit door is operative and ON when requireed.

4. When any of the cameras 2, 3, inoperataive, another flight attendant must assure that the crew

member/flight crew member required to enter thecockpit is not followed by passenger(s).

Note:

Any portion of the system which is

operative may be used.

12 FEB 12MEL

A320/321MEL/CDL 01.23.13

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-01 Cabin

Intercommunicatio

n Data System

(CIDS)

23-73-01-01Cabin

Intercommunicatio

n Data System

(CIDS) Function

23-73-01-01A 1 1 (M) The CIDS function must be operative.

Note:

i. Failure of a single CIDS director is indicated

by a MAINTENANCE message on the

STATUS SD page.

Refer to Item 23-00-01 CIDS 1(2)

MAINTENANCE Message

ii. In the case of disturbance of the CIDS

function, the deactivation of the affected

CIDS director may recover normal operation

of the CIDS function.

Refer to AMM TASK 23-73-00-040-001



SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-02 DEU A

23-73-02-01 Cabin DEU A

23-73-02-01A C 21 0 (O) One or more may be inoperative and affected passenger

seat may be occupied provided that :

1) The passenger announcement can be heardthroughout the cabin during the flight, and

2) The passenger address system is used to alert thepassengers when "Return to Seat / Fasten Seat Belt /No Smoking" signs are requested.


GENERAL INFORMATION

On the affected cabin area:

- general cabin illumination is set to full brightness,

- Passenger Call is not available,

- The (No Smoking/Fasten Seat Belt/No PortableElectric Device) Signs are not available.

IN FLIGHT

- When return to seat is requested,

or

When seat belts should be fasten,

or

When smoking is prohibited,

or

When portable electric device use is prohibited,

Use the passenger address system to alert cabinattendants and passengers.

12 FEB 12MEL

A320/321MEL/CDL 01.23.15

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-02 DEU A

23-73-02-01 Cabin DEU A

23-73-02-01B C 21 0 (FD) One or more may be inoperative provided that the affected

seats are blocked and placarded inoperative.

23-73-02-02 Lavatory DEU A

23-73-02-02A C 3 2 (FD) May be inoperative provided that the affected lavatory is

closed and placarded inoperative.

NOTE:

In case foreword lavatory placarded

extra pilot should be assigned to

operate the flight as a safety pilot to

relieve the pilot when leaving the cockpit

for personal reasons.

23-73-03 DEU B

23-73-03-01 Cabin DEU B

23-73-03-01B C 18 0 (O) One or more may be inoperative provided that:

1) One DEU B and the associated handset are operativeat each pair of floor level exit doors, and

2) The slide bottle pressure and door bottle pressureassociated with each affected DEU B are checked onthe associated direct reading pressure gauge beforethe first flight of each day, and




SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-03 DEU B

23-73-03-01 Cabin DEU B

23-73-03-01B (cont’d) 3) The associated lavatory fire extinguisher system ischecked operative, and

4) The absence of smoke in the affected lavatory isperiodically checked.Refer to Item 25-62-06 Passenger Door SlidePressure Message on the PTP/FAP (If Installed), and Refer to Item 52-10-06 DOOR PRESS LOW/CHECK DOOR PRESSURE Message on the PTP/FAP, and Refer to Item 26-17-01 Lavatory Smoke DetectionSystem.


PIC will brief cabin crew for the use of one cabin handset

per pair of floor level exit doors, if necessary. Define the

cabin handset location to be used by the purser, if

necessary.

12 FEB 12MEL

A320/321MEL/CDL 01.23.17

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-04 Cabin Individual

Call

23-73-04-01 Passenger Call


23-73-05 Cabin

Loudspeaker

23-73-05-01 Cabin

Loudspeaker

23-73-05-01A C 42 0 (FD) One or more may be inoperative provided that no seat is

occupied from which a passenger cannot hear a

passenger announcement.



SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-05 Cabin

Loudspeaker

23-73-05-02 Lavatory

Loudspeaker

23-73-05-02A C 3 0 (O)(FD) One or more may be inoperative provided lavatory is not

used for passengers.

It may used by crew member.


Flight attendant must be briefed to assure that affected

lavatory is not used by any passenger.

23-73-06 Handset

23-73-06-01 Cockpit Handset

23-73-06-01A C 1 0 May be inoperative provided that the cockpit audio controlpanel (ACP) is used for the communication between the

cockpit and the cabin.

23-73-06-02 Cabin Handset

23-73-06-02A (A320)

(A321)

C

C

3

5

2

4

(O) One may be inoperative provided that one handset is

operative at each pair of floor level exit doors.


1. The PIC in his briefing must inform all crew members

wich handset(s) is/are inoperative and the affectedflight attendant(s) should use the next availableoperative station or communicat in person when theneed arises.

2. FAIC must be seated in aposition having an operativehandset during Takeoff & Landing.

12 FEB 12MEL

A320/321MEL/CDL 01.23.19

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-06 Handset

23-73-06-03 Cabin Handset

Key

23-73-06-03A Passenger

address and

Cabin to cockpit

interphone

operative

(A320)

(A321)

C

C

3

5

1

3

One or more may be inoperative provided that:

1) Passenger address from the affected handset isoperative, and

2) Cabin to cockpit interphone from affected handset isoperative.

23-73-06-03B Refer to Item 23-73-06-02 Cabin Handset

23-73-07 Prerecorded

Announcement

and Music

Reproducer

(PRAM)

23-73-07-01 Prerecorded

Announcement

and Music

Reproducer

(PRAM)

23-73-07-01A C 1 0 (O) May be inoperative.


Procedure to replace the perecorded announcement must

be established and necessary demonstation equipment

must be provided onboard.



SEQUENCE


I T E M



MEL

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-08 Cabin

Assignment

Module (CAM)

23-73-08-01 Cabin

Assignment

Module (CAM)

23-73-08-01A C 1 0 May be inoperative or missing.

23-73-10 Smoke Detection

Function

23-73-10-01 Smoke Detection

Function (CIDS-

SDF)

23-73-10-01A C 1 0 (FD) May be inoperative provided that:

1) The cargo compartments are empty or do not containflammable or combustible materials, and

2) The lavatory smoke detection system is consideredinoperative.Refer to Item 26-17-01 Lavatory Smoke DetectionSystem

Note:

Failure of a single CIDS-SDF channel is

indicated by a MAINTENANCE

message on the STATUS SD page.

Refer to Item 26-00-01 SDCU/SMOKE

MAINTENANCE Message

12 FEB 12MEL

A320/321MEL/CDL 01.23.21

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-73 Cabin

Intercommunication

Data System

23-73-10 Smoke Detection

Function

23-73-10-01 Smoke Detection

Function (CIDS-

SDF)

23-73-10-01B C 1 0 May be inoperative provided that the restrictions

concerning lavatory smoke detection system and cargo

smoke detection system are applied.

Refer to Item 26-17-01 Lavatory Smoke Detection System,

and

Refer to Item 26-16-01 Smoke Detector in the FWD Cargo

Compartment (if FWD cargo compartment smoke

detection system installed) and

Refer to Item 26-16-02 Smoke Detector in the AFT and the

BULK Cargo Compartments (if AFT cargo compartmentsmoke detection system installed).

Note:

Failure of a single CIDS-SDF channel is

indicated by a MAINTENANCE

message on the STATUS SD page.


MAINTENANCE Message



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-74 Cabin Crew Panel

23-74-01 FAP Display Unit

23-74-01A C 1 0 (O) May be inoperative provided that the safety related

messages on the FAP are considered inoperative.

Refer to Item 52-10-06 DOOR PRESS LOW/CHECK

DOOR PRESSURE Message on the PTP/FAP, and

Refer to Item 25-62-06 Passenger Door Slide PressureMessage on the PTP/FAP (If Installed), and

Refer to Item 25-62-07 Emergency Exit Slide Pressure

Message on the PTP/FAP


GENERAL INFORMATION

The cabin lighting may be dimmed through the Additional Attendant Panel (AAP) (If available).

23-74-02 EMER pb on

Hardkey FAPSub-panel


23-74-03 Other Controls

on Hardkey FAP

Sub-panel

23-74-03A D 1 0 May be inoperative.

23-74-06 Door Bottle

Pressure

Monitoring on

the FAP

23-74-06A (A320)

(A321)

C

C

4

8

0

0

Refer to Item 52-10-06 DOOR PRESS LOW/CHECK

DOOR PRESSURE Message on the PTP/FAP

12 FEB 12MEL

A320/321MEL/CDL 01.23.23

COMMUNICATIONS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATIONS

23-74 Cabin Crew Panel

23-74-08 Slide Pressure

Monitoring on the

FAP

23-74-08A Refer to Item 25-62-06 Passenger Door Slide Pressure


Refer to Item 25-62-07 Emergency Exit Slide Pressure


Note:

Apply both MEL Items.

23-74-09 Area Call Panel


23-74-10 Attendant

Information Panel

(AIP)


23-74-11 Additional

Attendant Panel

(AAP)


* * *



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-00 MAINTENANCE

Messages on the

STATUS SD page

24-00-01 DC BUS TIE

MAINTENANCE

Message

24-00-01A C 1 - DC BUS TIE MAINTENANCE message may be displayed

on the STATUS SD page.

24-00-03 AC GEN

MAINTENANCE

Message

24-00-03A C 1 - AC GEN MAINTENANCE message may be displayed on

the STATUS SD page.


24-01-01 ELEC Overhead

Panel

24-01-01-01 BAT 1(2) pb-sw

FAULT light


24-01-01-02 BAT 1(2) pb-sw

OFF light


24-01-01-03 GEN pb-sw

FAULT light and

APU GEN pb-swFAULT light

24-01-01-03A C 3 1 One GEN pb-sw FAULT light and/or the APU GEN pb-sw

FAULT light may be inoperative provided that the

associated generator indications are operative on the

ELEC SD page.

12 FEB 12MEL

A320/321MEL/CDL 01.24.01

ELECTRICAL POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER



Panel

24-01-01-04 GEN pb-sw OFF

light and APU

GEN pb-sw OFF

light


24-01-01-05 AC ESS FEED

pb-sw FAULT

light

24-01-01-05A C 1 0 May be inoperative provided that the AC ESS bus

indication is operative on the ELEC SD page.

24-01-01-06 AC ESS FEED

pb-sw ALTN

light

24-01-01-06A C 1 0 May be inoperative provided that the AC ESS bus

indication is operative on the ELEC SD page.

24-01-01-07 EXT PWR pb-sw

AVAIL light



BEFORE PUSHBACK

Confirm the external power disconnection either on the

ELEC SD page or with the ground crew.

PARKING

- If the APU is not available:

- EXT PWR pb-sw. . . . . . . . . . . . . . . . . . . . . . . . ON

- Confirm the external power connection either on

the ELEC SD page or with the ground crew before

engine shutdown.



SEQUENCE


01.24.02ELECTRICAL POWER


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER



Panel

24-01-01-08 EXT PWR pb-sw

ON light


24-01-01-09 GALY & CAB pb-

sw FAULT light

24-01-01-09A C 1 0 (O) One may be inoperative provided that:

1) For each generator, the AC load indication is operativeon the ELEC SD page, and

2) The GALY & CAB automatic load shed system ischecked operative.



Check of the galley automatic load shed system:

- Supply the electrical network from the APU or theexternal power.

- GALY & CAB pb-sw · · · · · · · · · · · · · · · · · · · · · · AUTO

- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull

- Check that a part of the operative galley equipmentdoes not operate.

- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push

Note:

Disregard this procedure if main galleys

are not connected.

12 FEB 12MEL

A320/321MEL/CDL 01.24.03

ELECTRICAL POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER



Panel

24-01-01-10 GALY & CAB pb-

sw OFF light


24-01-01-11 COMMERCIAL

pb-sw OFF light


24-01-01-12 BUS TIE pb-sw

OFF light


24-01-01-13 IDG pb-sw

FAULT light

24-01-01-13A C 2 1 One may be inoperative provided that the frequency and

the temperature indications of the affected generator are

operative on the ELEC SD page.

24-01-02 EMER ELEC

PWR Overhead

Panel

24-01-02-01 RAT & EMER

GEN FAULT

light

24-01-02-01A B 1 0 May be inoperative.



SEQUENCE




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-07 Indications on the

ELEC SD page

24-07-01 AC Generation

Indications on

the ELEC SD

page

24-07-01A C 3 0 (O) One or more indications related to the AC generation may

be inoperative provided that:

1) The load, voltage, and frequency indications areoperative on one engine driven generator , and

2) The associated ELEC GEN 1(2) FAULT alert isoperative, and

3) The galley automatic load shed system is checkedoperative.



Check that GEN 1(2) pb-sw FAULT light is on (with the

GEN 1(2) pb-sw in the on position).






- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)

C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push

Note:


are not connected.


12 FEB 12MEL

A320/321MEL/CDL 01.24.05

ELECTRICAL POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER


ELEC SD page

24-07-02 DC Generation

Indications on

the ELEC SD

page (Cont’d)

24-07-02A C 2 0 One or more indications related to the DC generation may

be inoperative.

24-07-03 AC ESS BUS

SHED Indication

on the ELEC SD

page

24-07-03A C 1 0 May be displayed.

24-09 ECAM Alerts

24-09-01 ELEC AC ESS

BUS SHED Alert

24-09-01A C 1 0 (O) May be displayed provided that:


2) The AC ESS BUS SHED is checked operative beforeeach flight, and

3) HF 1 is deactivated.

Refer to Item 23-10-01 HF System


GENERAL INFORMATION

When the ELEC AC ESS BUS SHED alert is displayed onthe EWD:

- The AC ESS BUS SHED message may appear on theELEC SD page,

- The CAPT AOA message may be displayed in theINOP SYS column on the STATUS SD page,




SEQUENCE




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-09 ECAM Alerts

24-09-01 ELEC AC ESS

BUS SHED Alert


- The ELEC/AC BUS/8XP/MONG (49VU H11) C/B maytrip.


COM/HF1 (49VU HA14) C/B · · · · · · · · · · · · · · · · · Pull

Check of the AC ESS BUS SHED:- Supply the electrical network from the APU or the

external power.

- Check that the CAPT right DU is operative.

IN FLIGHT

- If either the ANTI ICE F/O AOA alert or the ANTI ICEF/O PROBES alert is displayed on the EWD, andicing conditions cannot be avoided:- ADR 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

- AIR DATA sw . . . . . . . . . . . . . . . . . . . . . . . . . . F/O 3

Note:

If the ADR 2 pb-sw is set to OFF, takeoff

in CONF 1+F is not permitted.

- If either the ANTI ICE STBY AOA alert or the ANTIICE STBY PROBES alert is displayed on the EWD,and icing conditions cannot be avoided:

ADR 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

24-09-02 C/B TRIPPED

Alert

24-09-02A C 1 0 (M) May be displayed provided that the alert is confirmed to be

false by troubleshooting.


Refer to AMM 24-50-00-040-001

12 FEB 12MEL

A320/321MEL/CDL 01.24.07

ELECTRICAL POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-22 AC Main Generation

24-22-01 AC Main

Generation (IDG,

GCU, Line

Contactor)

24-22-01A B 2 1 (O)(M)

(FD)


1) The flight altitude is limited to 33 000 ft, and

2) The APU and AC auxiliary generation are operativeand used throughout the flight, and

3) The APU fuel pump is operative, and

4) The APU oil consumption is checked adequate for theintended flight, and

5) All busses have power, and

6) The indications and alerts for the remaining AC maingeneration and the AC auxiliary generation areoperative, and

7) The galley automatic load shed system is checkedoperative.



landing capability is CAT II.

APU fuel consumption with APU GEN pb-sw On:

Note:

When the External Power isdisconnected, the IFE is lost until the

APU supplies the electrical network.




SEQUENCE




MEL

I T E M

FL GND 200 250 300 335 390

KG/H 100 63 57 54 49 42



SEQUENCE


7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-22 AC Main

Generation

24-22-01 AC Main

Generation (IDG,

GCU, Line

Contactor)








- ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24)C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push

Note:


are not connected.


12 FEB 12MEL

A320/321MEL/CDL 01.24.09

ELECTRICAL POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-22 AC Main Generation

24-22-01 AC Main

Generation (IDG,

GCU, Line

Contactor)


AFTER ENGINE START

Check that the electrical busses have power:

- APU MASTER SW pb-sw · · · · · · · · · · · · · · · · · · · · ON

- APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- GEN 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- GEN 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- On the ELEC SD page, check that all AC busses havepower.

- GEN pb-sw (operative)· · · · · · · · · · · · · · · · · · · · · · · On

- APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- On the ELEC SD page, check that all AC busses havepower.

- APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · On

Note:

If necessary, the IDG may be

disconnected.

CAUTION

For economical reason, the IDG should

not operate for more than 50 flight hours

in the disconnected mode.


Refer to AMM 24-20-00-040-001



SEQUENCE



A320321MEL/CDL 12 FEB 12

MEL

I T E M



SEQUENCE


7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-22 AC Main

Generation

24-22-02 AC Bus Tie

Control Function


24-23 AC Auxiliary

Generation

24-23-01 AC Auxiliary

Generation (APU

Generator, GCU,

Line Contactor)

Note:

When the GPCU and the APU

Generator are both inoperative, the

engines cannot be started.

24-23-01A C 1 0 May be inoperative provided that the APU GEN pb-sw is

set to OFF.

24-23-01B A 1 0 May be inoperative for four flights provided that the APU

GEN pb-sw is set to OFF.

24-24 AC EmergencyGeneration

24-24-01 Emergency

Generator


24-24-02 RAT Extension

Automatic

Control

24-24-02A B 1 0 (M) May be inoperative provided that the RAT extension

manual control is checked operative every day.


Refer to AMM 24-20-00-040-002

12 FEB 12MEL

A320/321MEL/CDL 01.24.11

ELECTRICAL POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-24 AC Emergency

Generation

24-24-03 RAT Extension

Manual Control

24-24-03A B 1 0 May be inoperative.

24-25 AC Essential

Generation

Switching

24-25-01 Manual Transfer

to the AC BUS 2

(ALTN Function)


1) The AC ESS FEED pb-sw is set to NORM, and

2) It is checked on the ELEC SD page that the AC BUS 1supplies the AC ESS BUS, and

3) The TR 2 is operative.


DURING PRELIMINARY COCKPIT PREPARATION

On the ELEC SD page, check that the AC BUS 1supplies the AC ESS BUS.

24-25-02 Automatic

Transfer to the

AC BUS 2


1) The AC ESS FEED pb-sw is set to NORM, and2) It is checked on the ELEC SD page that the AC BUS 1

supplies the AC ESS BUS, and

3) The TR 2 is operative.




SEQUENCE




MEL

I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-24 AC Emergency

Generation

24-25-02 Automatic

Transfer to the

AC BUS 2



On the ELEC SD page, check that the AC BUS 1supplies the AC ESS BUS.

24-26 Galley and

Commercial

Supply System

24-26-01 GALY & CAB

Automatic Load

Shed System

24-26-01A Manual Load

Shed System

Operative

C 1 0 May be inoperative provided that the manual load shed

system and the GALY & CAB pb-sw FAULT light are

operative.

24-26-01B All GALY &

CAB Loads

disconnected

C 1 0 (M) May be inoperative provided that all GALY & CAB loads

are disconnected.


Refer to AMM 24-56-00-040-001

12 FEB 12MEL

A320/321MEL/CDL 01.24.13

ELECTRICAL POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-26 Galley and

Commercial Supply

System

24-26-02 GALY & CAB

Manual Load

Shed System

(GALY & CAB

pb-sw)

24-26-02A All GALY &

CAB loads

disconnected

C 1 0 (M) May be inoperative provided that all GALY & CAB loads

are disconnected.


Refer to AMM 24-56-00-040-002

24-26-02B COMMERCIAL

supply system

operative

C 1 0 (O)(M) May be inoperative provided that the COMMERCIAL

supply system is checked operative.


ON GROUND OR IN FLIGHT

- If the AVNCS SMOKE emergency procedure isapplied or if the AVIONICS SMOKE alert isdisplayed on the EWD replace the action to set theGALY & CAB pb-sw to OFF by the followingactions:- EMER EXIT LT selector. . . . . . . . . . . . As required

- COMMERCIAL pb-sw . . . . . . . . . . . . . . . . . . . OFF

Note:

When the COMMERCIAL pb-sw is set

to OFF, the normal cabin lighting goes

off.Minimum cabin lighting is recovered

when the EMER EXIT LT selector is set

to ON.


Refer to AMM 24-51-00-040-001



SEQUENCE




MEL

I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-26 Galley and

Commercial

Supply System

24-26-03 Commercial

Supply System




- If the AVNCS SMOKE emergency procedure isapplied or if the AVIONICS SMOKE alert isdisplayed on the EWD replace the action to set theCOMMERCIAL pb-sw to OFF by the followingactions:- BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

- GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

The F/O PFDU, the F/O NDU, and the ECAM lower display are lost.- If the smoke persists:

- GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

When the GEN 2 pb-sw is set to on, all the

electrical busses are recovered but the TR 2

remains inoperative

- BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

Before the landing gear extension:

- GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On

When the GEN 2 pb-sw is set to on, all the electrical

busses are recovered but the TR 2 remains

inoperative

- BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

24-28-01 Static Inverter

AC Generation


12 FEB 12MEL

A320/321MEL/CDL 01.24.15

ELECTRICAL POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-32 DC Main Generation

(TR 1, TR 2)

24-32-01 DC Main

Generation (TR

1, TR 2)

24-32-01A TR1 inoperative A 2 1 (O)(FD) TR 1 may be inoperative provided repairs are made within

two flight days.





TR 1/CNTOR/SPLY (125VU CF01) C/B· · · · · · · · · Pull

On the ELEC SD page, check that the TR 2 and theESS TR voltages are both equal to or above 27 V.On the battery voltage indicator, check that the BAT 1and the BAT 2 voltages are both equal to or above25.5 V.

The batteries must be set to OFF during this check.

24-32-01B TR 2 inoprative A 2 1 (O)(M)

(FD)

TR 2 may be inoperative provided that:

1) The AC ESS FEED control is checked operative everyday, and

2) The ISIS airspeedindication is operative, and

3) The ISIS altitude indication is operative, and

4) The ISIS aircraft attitude indication is operative, and

5) The standby compass is operative, and

6) Repairs are made with two flight days.







SEQUENCE




MEL

I T E M

7/23/2019 A 320321 Mel Cdl


24 ELECTRICAL POWER

24-32 DC Main

Generation (TR 1,

TR 2)

24-32-01 DC Main

Generation (TR

1, TR 2)

24-32-01B (Cont’d) OPERATING PROCEDURES(Cont’d)


TR 2/CNTOR/SPLY (124VU BC01) C/B· · · · · · · · · Pull

On the ELEC SD page, check that the TR 1 and theESS TR voltages are both equal to or above 27 V.On the battery voltage indicator, check that the BAT 1and the BAT 2 voltages are both equal to or above25.5 V.The batteries must be set to OFF during this check.

AC ESS FEED pb-sw · · · · · · · · · · · · · · · · · · · · · ALTN

IN FLIGHT

- In the case of failure of the AC BUS 2, all DUs are

lost. In this case: AC ESS FEED pb-sw· · · · · · · · · · · · · · · · · · · · · · Norm

- In the case of failure of the AC BUS 1:

RAT MAN ON pb-sw (on HYD overheadpanel)....................................................................Set


Refer to AMM 24-30-00-040-002

24-34 DC Emergency

Generation (ESS

TR)

24-34-01 DC Emergency

Generation (ESS

TR)


12 FEB 12MEL

A320/321MEL/CDL 01.24.17

ELECTRICAL POWER



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24 ELECTRICAL POWER

24-35 DC Essential and

Normal Generation

Switching

24-35-01 DC TIE

Contactor 1PC1

(DC BUS 1-DC

BAT BUS), 4PC

(DC ESS BUS-

DC BAT BUS)

24-35-01A C 2 1 One may be inoperative in the open position.

24-35-02 DC TIE

Contactor 1PC2

(DC BUS 2-DC

BAT BUS)


24-38 DC Battery

Generation

24-38-01 BAT 1(2)

Channel




SEQUENCE




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24 ELECTRICAL POWER

24-38 DC Battery

Generation

24-38-02 Battery Charger

Limiter (BCL)

24-38-02A A 2 1 (O)(M)

(FD)

One may be inoperative for 10 flights provided that:

1) No APU start is attempted neither on ground nor inflight, and

2) Both AC main generations are operative, and

3) The refueling is made with an external power unitconnected, and

4) The battery associated with the inoperative BCL ischarged before each flight.



Do not use the APU.

Use a ground power unit to start the engines onground.


- If BAT 1 is affected:

BAT 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- If BAT 2 is affected:

BAT 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF


Refer to AMM 24-30-00-040-001

24-38-03 Battery

Voltmeter

24-38-03A C 2 0 One or both may be inoperative provided that the

associated voltage indication is operative on the ELEC SD

page.

12 FEB 12MEL

A320/321MEL/CDL 01.24.19

ELECTRICAL POWER



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24 ELECTRICAL POWER

24-41 AC External Power

Control

24-41-01 Ground Power

Control Unit

(GPCU)

24-41-01A C 1 0 May be inoperative provided APU Generator is operative.

Note:




24-41-02 External Power

Receptacle

24-41-02A C 1 0 (M) May be inoperative provided that the receptacle is

placarded inoperative and not used.

Note:





Refer to AMM 24-41-00-040-001

* * *



SEQUENCE




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25 EQUIPMENT/FURNISHINGS


DOOR/OXY SD

page

25-07-01 Passenger Door

Slide Permanently

Indicated Armed

(A320)

(M) Note:

The correct indication may be recovered

by performing the AMM task 52-70-00-

040-07.

25-07-01A C 4 0 (O) One or more may be permanently indicated in the armed

position provided that the associated slide is visually

checked to be armed before each flight.


ON GROUND

Cabin crew must confirm before each flight that the

associated slide is armed.

25-07-01 Cabin Passenger Door / Emergency

Exit Slide

Permanently

Indicated Armed

(A321)

(M) Note:



040-07.

25-07-01A C 8 0 (O) One or more may be permanently indicated in the armed

position provided that the associated slide is visually

checked to be armed before each flight.


ON GROUND



12 FEB 12MEL

A320/321MEL/CDL

01.25.01EQUIPMENT/

FURNISHINGS



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DOOR/OXY SD page


Slide Permanently

Indicated Not

Armed

(A320)

(M) Note:



040-07.

25-07-02A Associated

door

considered

operative

C 4 0 (O)(FD) One or more may be permanently indicated in the not

armed position provided that:

1) The aircraft is not operated at night, and

2) The associated slide is visually checked to be armedbefore each flight.


ON GROUND



25-07-02 Cabin Passenger Door / Emergency

Exit Slide

Permanently

Indicated Not

Armed

(A321)


door

considered

operative

C 8 0 (O)(FD) One or more may be permanently indicated in the not



2) The associated slide is visually checked to be armed

before each flight.


ON GROUND



01.25.02EQUIPMENT/FURNISHINGS


MEL



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DOOR/OXY SD

page

25-07-03 Overwing

Emergency Exit

Slide Permanently

Indicated Armed

Note:



040-07.

25-07-03A C 2 0 (M) One or both may be permanently indicated in the armedposition provided that the associated slide is visually

checked to be armed before the first flight of the day.


Refer to AMM 52-70-00-040-008

25-07-04 Overwing

Emergency Exit

Slide Permanently

Indicated NotArmed

Note:



040-07.

25-07-04A Overwing

emergency

exits

considered

operative

C 2 0 (M)(FD)One or both may be permanently indicated in the not



2) The associated slide is visually checked to be armedbefore the first flight of the day.


Refer to AMM 52-70-00-040-009

12 FEB 12MEL

A320/321MEL/CDL

01.25.03EQUIPMENT/

FURNISHINGS



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25-11 Pilot Seats

25-11-01 Pilot Seat Manual

Horizontal

Adjustment


25-11-02 Pilot Seat Manual

Vertical

Adjustment


electrical

control

operative

C 2 0 One or both may be inoperative provided that the

associated electrical control is operative.

25-11-02B Associated

electrical

control

inoperative

C 2 0 One or both may be inoperative provided that the seating

position is acceptable to the affected crewmember.

25-11-03 Pilot Seat ReclineAdjustment

25-11-03A C 2 0 (M) One or both may be inoperative provided that the seat is

secured in an upright position acceptable to the affected

crewmember.


Refer to AMM 25-11-00-040-001

25-11-04 Pilot Seat Other

Manual

Adjustments

25-11-04A C 2 0 One or more may be inoperative provided that the seating

position is acceptable to the affected crewmember.



MEL



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25-11 Pilot Seats

25-11-05 Pilot Seat

Electrical

Adjustment

25-11-05A C 2 0 (M) One or both may be inoperative provided that the electrical

adjustment of the associated seat is deactivated.


Refer to AMM 25-11-00-040-002

25-11-06 Pilot Seat

Shoulder Harness

25-11-06A A 2 1 (O)(FD) May be inoperative on the F/O seat for three flights.


BEFORE TAKEOFF

The takeoff briefing should include the status of the

affected seat and the position to be adopted by the F/O in

the case of RTO.

To cope with any potential RTO:

The F/O must tightly fasten operative harness strap.

DURING FLIGHT

For any phase of flight in turbulence atmosphere:

The F/O must fasten the belts accordingly.

BEFORE LANDING

The landing briefing should include the status of theaffected seat and the position to be adopted by the F/O in

the case of high deceleration at landing.

To cope with any potential high deceleration at landing:

The F/O must tightly fasten operative harness straps.

12 FEB 12MEL

A320/321MEL/CDL

01.25.05EQUIPMENT/

FURNISHINGS



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25-11 Pilot Seats

25-11-07 Pilot Seat Fifth

Strap

25-11-07A C 2 0 (O) One or both may be inoperative.


DURING FLIGHT

To cope with any potential turbulence situation:

The crewmember of the affected seat must tightly fasten

the operative harness straps.

25-11-08 Pilot Sidestick

Armrest Height

Adjustment

25-11-08A C 2 1 One may be inoperative provided that the associated

armrest position is acceptable to the affected

crewmember.


Armrest Pitch

Adjustment


armrest position is acceptable to the affected

crewmember.


Armrest Memory

Position Display




MEL



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25-11 Pilot Seats

25-11-11 Pilot Inboard

Armrest Vertical

Adjustment


25-11-12 Pilot Seat

Headrest


25-12 Third and Fourth

Occupant Seats

25-12-01 Third Occupant

Seat

25-12-01A Seat stowed C 1 0 (FD) May be inoperative provided that the seat is in its stowed

position.

25-12-02 Third OccupantSeat Shoulder

Harness

25-12-02A C 1 0 (FD) May be inoperative provided that the seat is not occupied

during takeoff and landing.

12 FEB 12MEL

A320/321MEL/CDL

01.25.07EQUIPMENT/

FURNISHINGS



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Occupant Seats


Seat Abdominal

Belt

25-12-03A C 1 0 (FD) May be inoperative provided that:

1) The seat is placarded inoperative, and

2) The seat is not occupied.


Seat Fifth Strap



With any potential turbulance situation the crewmember

must lightly fasten the operative straps.


Seat

25-12-05A Seat stowed C 1 0 May be inoperative provided that the seat is in its stowed

position.


Seat Shoulder

Harness

25-12-06A C 1 0 (FD) May be inoperative provided that the seat is not occupied

during takeoff and landing.


Seat Abdominal

Belt

25-12-07A C 1 0 (FD) May be inoperative provided that:

1) The seat is placarded inoperative, and

2) The seat is not occupied.



MEL



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Occupant Seats


Seat Fifth Strap

25-12-08A D 1 0 (O) May be inoperative.


With any potential turbulance situation the crewmember must lightly fasten the operative straps.

25-13 Lining and

Furnishings

25-13-01 Pilot Sliding Table

25-13-01A Table stowed C 2 0 One or both may be inoperative in its stowed position.

25-13-02 Pilot Retractable

Footrest

25-13-02A Footreststowed

C 4 0 One or more may be inoperative in its stowed position.

25-20 Cabin Seats

25-20-01 Passenger Seat

25-20-01A (A320)

(A321)

C

C

C

132

116

165

86

70

100

(FD) May be inoperative provided:

a) Seat does not block and Emergency Exit,

b) seat does not restrict any passenger from access tothe main aircraft aisle, and

c) Affected seat(s) are blocked and placarded “DO NOTOCCUPY”.

Note 1:

A seat with an inoperative seat belt is



12 FEB 12MEL

A320/321MEL/CDL

01.25.09EQUIPMENT/

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25-20 Cabin Seats

25-20-01 Passenger Seat

25-20-01A (Cont’d) Note 2:

Inoperative seats do not affect the

required number of Flight Attendants.

Note 3:

Affected seat(s) may include the seat(s)

behind and/or adjacent outboard seats.

25-20-03 Cabin Attendant

Seat

Note:

A cabin attendant seat with aninoperative or missing seat belt or

harness should be considered

inoperative.




MEL



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25-20 Cabin Seats


Seat (cont’d)

25-20-03B Required

cabin

attendant seat

(A320)

(A321)

C

C

5

7

4

5

(O)(M)

(FD)

One required cabin attendant seat may be inoperative or

not usable provided that:

1) The cabin attendant assigned to affected seatoccupies a passenger seat as close to or closer than

nearest seated passenger to the associated exit, and2) The passenger seat to be used by cabin attendant is

correctly placarded, and

3) The cabin attendant can reach assigned exit andemergency equipment in nearly the same time as fromnormally assigned seat, and

4) The direct view of passenger cabin by flight attendantsis not impaired, and

5) The alternate procedures are established for displacedflight attendant according to national regulations, and

6) The affected seat is secured in its stowed position or

removed.OPERATING PROCEDURES

Captin brief all cabin crew regarding the passenger seat

that occupie by assigned flight attendant.


Refer to AMM 25-22-00-040-001

01 MAY 12MEL

A320/321MEL/CDL

01.25.11EQUIPMENT/

FURNISHINGS



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25-28 Overhead Storage

25-28-01 Overhead Storage

Bin(s)/Cabin and

Galley storage

Compartment/

Closets

25-28-01A (A320)

(A321)

C

C

74

87

68

80

(M) May be inoperative provided:

a) Associated bin or compartment is placarded DO NOTUSE,

b) Any emergency equipment located in affectedcompartment is removed or considered inoperative,and

c) Cabin crew must be notified

NOTE:

These provisions are not intended to

prohibit inspections by crew members.


Refer to AMM 25-20-00-040-001

25-35 Galley Equipment

25-35-01 Galley Waste

Compartment

Flapper Door

25-35-01A C 3 0 (O)(M) One or more may be inoperative or missing provided that:

1) The galley waste compartment is empty, and

2) The associated access is secured in the closedposition to prevent waste introduction.

Note:

Non-safety related galley equipment is

not listed in this MEL.




MEL



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25-35 Galley Equipment

25-35-01 Galley Waste

Compartment

Flapper Door


Inform cabin crew to essure adequate galley waste

storage capacity is maintained during periods of flightwhen affected containers are secured empty.


Refer to AMM 25-35-00-040-001

25-40 Lavatories

25-40-01 Toilet Waste

Compartment

Flapper Door

25-40-01A C 3 2 (O)(M)(FD) One may be inoperative or missing provided that:1) The toilet waste compartment is empty, and

2) The associated access is secured in the closedposition to prevent waste introduction.

Note:

Non-safety related toilet equipment is

not listed in this MEL.


- Lavatory door placarded “INOPERATIVE-DO NOTENTER”.

- Lavatory is used only by crew members.

- Ensure that affected lavatory is kept locked and is notentered exept for crew member.


Refer to AMM 25-40-00-040-001

12 FEB 12MEL

A320/321MEL/CDL

01.25.13EQUIPMENT/

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25-40 Lavatories

25-40-02 Exterior Lavatory

Ashtray

25-40-02A D 4 0 One or more may be damaged or missing provided that

the flight is non-smoking.

25-40-03 Interior Lavatory

Ashtray

25-40-03A Lavatory fire

extinguishing

system

operative

C 3 0 One or more may be damaged or missing provided that

the associated lavatory fire extinguishing system is

operative.

25-40-03B Lavatory

locked closed

C 3 2 (FD) One may be damaged or missing provided t hat t he

associated lavatory is locked closed and placarded

inoperative.

25-50 CargoCompartments

25-50-01 Cargo Loading

System

25-50-01A D 2 0 (FD) May be inoperative provided Ramp Load Control

Supervisor must check and confirm to the flight crew that

cargo compartments are loaded normally.



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25-50 Cargo

Compartments

25-50-02 Decompression

Panels in the

Cargo

Compartments

25-50-02A C 23 0 (FD) One or more may be damaged or missing provided that

the associated cargo compartment is empty or does not

contain flammable or combustible materials.

25-50-03 Sidewall Linings

and Ceiling Panels

in the Cargo

Compartments

25-50-03A Damaged

panel

C 41 0 (FD) One or more may be damaged provided that the

associated cargo compartment is empty or does not


25-50-04 Cargo

CompartmentRestraint

Components

(Nets, Attach

Points,

Stanchions)

25-50-04A C 5 0 One or more may be missing or damaged provided that

the remaining operative ones are enough to secure the

load in the affected compartment.

12 FEB 12MEL

A320/321MEL/CDL

01.25.15EQUIPMENT/

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25-62 Cabin Escape

Facilities

25-62-01 Cabin Passenger

Door Slide or Slide

Raft

25-62-01A Slide

inoperative

4 4

25-62-02 Overwing

Emergency Exit

Slide or Slide Raft

(A320)

25-62-02A Slide

inoperative

2 2

25-62-03 Emergency ExitSlide or Slide Raft

(A321)

25-62-03A Slide

inoperative

4 4



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25-62 Cabin Escape

Facilities

25-62-04 SLIDE ARMED

light

(A320)

25-62-04A C 6 0 One or more may be inoperative provided maintenance

confirm that it’s only lit problem.

25-62-04 SLIDE ARMED

light

(A321)

25-62-04A C 8 0 One or more may be inoperative provided maintenance

confirm that it’s only lit problem.

25-62-05 Survival Kit

25-62-05A 4 4 Must be attached to each required life raft for over water

flying.

25-62-06 Passenger Door CHECK SLIDE

PRESSURE

Message on Flight

Attendant Panel

(FAP)

(A320)

25-62-06A C 4 0 (M) One or more messages may be displayed provided that

the slide bottle pressure is checked before the first MMEL

dispatch and then every 600 flight hours or every 4

months, whichever occurs first.


Refer to AMM 25-62-00-040-009

12 FEB 12MEL

A320/321MEL/CDL

01.25.17EQUIPMENT/

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25-62 Cabin Escape

Facilities


CHECK SLIDE

PRESSURE

Message on Flight

Attendant Panel

(FAP)

(A321)

25-62-06A C 8 0 (M) One or more messages may be displayed provided that

the slide bottle pressure is checked before the first MMEL

dispatch and then every 600 flight hours or every 4

months, whichever occurs first.


Refer to AMM 25-62-00-040-009

25-62-07 Overwing

Emergency Exit

CHECK SLIDE

PRESSUREMessage on Flight

Attendant Panel

(FAP)

(A320)

25-62-07A Check of the

slide bottle

pressure

C 2 0 (M) One or both messages may be displayed provided that the

associated slide bottle pressure is checked before the first

flight of each day.


Refer to AMM 25-62-00-040-005



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25-62 Cabin Escape

Facilities

25-62-08 Overwing Escape

Life Line

25-62-08B Non extended

overwater

flight

C 2 0 (FD) One or both may be inoperative or missing provided that

extended overwater flight is not conducted.

25-63 Evacuation

Signaling

Equipment

25-63-01 Emergency

Evacuation

Signaling System

(COMMAND pb-

sw, HORN SHUT

OFF pb,

CAPT&PURS andCAPT sw)

25-63-01A B 1 0 (O) May be inoperative.


GENERAL INFORMATION

If necessary, the information will be given through the

passenger address system or the cabin interphone

system.

12 FEB 12MEL

A320/321MEL/CDL

01.25.19EQUIPMENT/

FURNISHINGS



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25-64 First Aid Equipment

25-64-01 First Aid Kit

25-64-01A A 3 2 One may be incomplete, missing or used provided:

1) Affected FAK is identifiable as a unit that could not bemistaken for a fully serviceable unit, and

2) Repairs or replacements are made within 3 flightcycles.

Note:

- One serviceable Firs Aid Kit is required

on ferry flights.

- A first Aid Kit is considered serviceable

when Kit contains the following contents

Adhesive bandage compresses, 1-inch 16

Antiseptic swabs 20

Ammonia inhalants 10

Bandage compresses, 4-inch 8

Triangular bandage compresses, 4-inch 5

Arm splint, non inflatable 1Leg splint, non inflatable 1

Roller bandage, 4-inch 4

Adhesive tape, 1-inch standard roll 2

Bandage scissors 1

Protective latex gloves or equivalent nonpermeable gloves 1 Pair



MEL



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25-64 First Aid

Equipment

25-64-02 Emergency

Medical Kit

25-64-02A 1 1 Must be carried for all passenger flight. Must also be

carried for ferry flights where the aircraft is being

repositioned for a passenger flight.

Note:

Ferry flight terminating in JED do not

require the Doctor’s Emergency Kit. In

addition, ferry flight to other stations

besides Jeddah do not requir the

Doctor’s Emergency Kit if advance

coordination is none to ensure that a

Doctro’s Emergency Kit is available at

the terminatijng station to be installed

prior to the aircraft resuming passenger

service.

12 FEB 12MEL

A320/321MEL/CDL

01.25.21EQUIPMENT/

FURNISHINGS



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25-64-03 Automated

External

Defibrillator (AED)

25-64-03A 1 1 (M) Must be carried for all passenger flights.

MAINTENANCE PROCEDURES:

Refer to maintenance task.



MEL



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25-65 Emergency

Equipment

25-65-01 Cockpit Flashlight

25-65-01A C 4 0 May be inoperative or missing provided flight deck

member assigned to associated station has a flashlight

with equivalent characteristics readily available.

25-65-02 Cabin Flashlight

25-65-02A C 6 0 May be inoperative or missing provided cabin

crewmember assigned to associated seat has a flashlight

with equivalent characteristics readily available.

25-65-03 Crash

Axe/Crowbar

25-65-03A 1 1 Must be available.

25-65-04 Emergency

Locator

Transmitter (ELT)

25-65-04A Survival Type

ELTs

1 1

25-65-04B Fixed ELTs 1 1 Must be operative.

12 FEB 12MEL

A320/321MEL/CDL

01.25.23EQUIPMENT/

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25-65-05 Fireproof Gloves

25-65-05A All damaged

or missing

C 2 1 One may be damaged or missing.

25-65-05B One available 1 1 One must be available.

25-65-06 Megaphone

25-65-06A 2 2 Must be available and operative.

25-66 Floatation and

Survival Equipment

25-66-01 Life Vest

25-66-01A (A320)

(A321)

C

C

C

125

154

180

125

154

180

(FD) Life vest required for all over water flight , and a life vest

must be available for each passenger and crew on board.

25-66-02 Supplementary

Life Raft

25-66-02A C 1 1 (FD) Must be available for all over water flight.



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25-70 Non-Essential

Equipment &

furnishings

25-70-01 Non-Essential

Equipment &

furnishings (NEF)

25-70-01A D 17 9 (FD) Nonessential Equipment & Furnishings (NEF) are those

items installed on the aircrfaft as part of the original

certification, supplemental type certificate, or engineering

order that have no effect on the safe operation of flight and

would not be required by the applicable certification rules

or operational rules. They are those items that if

inoperative, damaged or missing have no effect on the

aircraft ability to be operated safely under all operational

conditions. these Nonessential items may be installed in

areas including, but not limited to, the passenger

compartment, flight deck area,service areas, cargo

areas,crew rest areas,lavatories, and galley areas. Items

addressed elsewhere in this MEL are not included.

25-70-01B25-70-01C

25-70-01D

25-70-01E

25-70-01F

25-70-01J

Coffee MakersOvens

Air Chillers

Hot Cups

Hot Jugs

Bun Warmers

DD

D

D

D

D

6

2

1

1

2

5 34

1

0

0

1

(FD) Any number or combination of galley equipment may beinoperative provided the in-flight supervisor/purser is

notified and determines that the operative galley

equipment available is adequate to support the associated

passenger service throughout the flight(s).

Note:

Captain will brief the FAIC of the

location of the inoperative galley

equipment, not to use the inoperative

galley equipment and that the

inoperative galley oven(s) must remain

empty.

12 FEB 12MEL

A320/321MEL/CDL

01.25.25EQUIPMENT/

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25-70 Non-Essential

Equipment &

furnishings

25-70-04 Movie/stereo

Equipment

25-70-04A D 1 0

25-70-05 Overhead Readig

Lamp

25-70-05A (A320)

(A321)

C

C

C

116

132

165

0

0

0

Any number may be inoperative

* * *



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26 FIRE PROTECTION

26-00 MAINTENANCE

Message on the

STATUS SD page

26-00-01 SMOKE

MAINTENANCE

Message

26-00-01A C 1 - SMOKE MAINTENANCE message may be displayed on

the STATUS SD page.


26-01-01 FIRE Overhead

Panel

26-01-01-01 Bulb/LED in the

ENG FIRE-PUSH

pb-sw

26-01-01-01A C 16 8 A maximum of four bulbs or LEDs may be inoperative in

each ENG FIRE-PUSH pb-sw.

26-01-01-02 ENG AGENT pb

DISCH light

26-01-01-02A One inoperative

on each engine

C 4 2 (M) One may be inoperative on each engine provided that the

associated bottle is checked before the first flight of each

day.


Refer to AMM 26-21-00-040-001

26-01-01-02B One inoperative

on one engine

A 4 2 (M) Both may be inoperative on one engine for four flights or

15 flight hours, whichever occurs first, provided that the

associated bottles are checked before each flight.


Refer to AMM 26-21-00-040-001



SEQUENCE


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.26.01

FIRE PROTECTION

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION



Panel

26-01-01-03 ENG AGENT pb

SQUIB light

26-01-01-03A C 4 2 (M) One may be inoperative for each engine provided Engine

extinguishing system firing circuit is checked operative

before the first flight of the day.


Refer to AMM 26-21-00-040-003

26-01-01-04 Bulb/LED in the

APU FIRE-PUSH

pb-sw

26-01-01-04A A maximum of

four bulbs or

LEDs

inoperative

C 8 4 A maximum of four bulbs or LEDs may be inoperative.

26-01-01-04B Five or more

bulbs or LEDs

inoperative

C 8 0 (M) Five or more bulbs or LEDs may be inoperative provided

that the APU is deactivated.

Refer to Item 49-10-01C Power Plant (APU)

26-01-01-05 APU AGENT pb

DISCH light

26-01-01-05A Check of bottle

pressure

C 1 0 (M) May be inoperative provided that the bottle is checked

before the first flight of each day.


Refer to AMM 26-22-00-040-004

26-01-01-05B APU

deactivated

C 1 0 (M) May be inoperative provided that the APU is deactivated.


01.26.02FIRE PROTECTION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION



Panel


SQUIB light

26-01-01-06A C 1 0 (M) May be inoperative provided that the APU extinguishing

system firing circuit is checked operative before the first

flight of each day.


Refer to AMM 26-22-00-040-005

26-01-01-06B C 1 0 (M) May be inoperative provided that the APU is deactivated.


26-01-01-31 ENG FIRE TEST

pb

26-01-01-31 C 2 1 (M) One may be inoperative provided that the associated

engine fire extinguishing and detection systems are

checked operative before the first flight of each day.


Refer to AMM 26-21-00-040-002

12 FEB 12MEL

A320/321MEL/CDL 01.26.03

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION



Panel

26-01-01-32 APU FIRE TEST

pb

26-01-01-32A Daily check C 1 0 (M) May be inoperative provided that the APU extinguishing

system firing circuit and the bottle low pressure detection

system are checked operative before the first flight of each

day.


Refer to AMM 26-22-00-040-012

26-01-01-32B APU

deactivated



26-01-01-33 APU FIRE PUSH

pb-sw

26-01-01-33A C 1 0 (M) May be inoperative provided that the APU is deactivated.



26-01-01-34A C 1 0 (M) May be inoperative provided that the APU is deactivated.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION


26-01-02 CARGO SMOKE

Overhead Panel

26-01-02-01 CARGO SMOKE

DISCH light

26-01-02-01A Check of bottle

weight

C 2 0 (M) May be inoperative provided that the associated bottle

weight is checked before the first flight of each day.


Refer to AMM 26-23-00-040-001

26-01-02-01B Associated

bottle

considered

inoperative

B 2 1 May be inoperative provided that the associated bottle is


Refer to Item 26-23-01 Cargo Agent Bottle

26-12 Engine Fire and

Overheat

Detection

26-12-01 Engine Fire

Detection Loop

A on the

Engine 1

26-12-01 C 1 0 One may be inoperative provided that:

1) The associated detection loop B is operative, and

2) The engine fire test is made before each flight.


Detection Loop

A on the

Engine 2

26-12-02 C 1 0 May be inoperative provided that the engine fire test is

made before each flight.

12 FEB 12MEL

A320/321MEL/CDL 01.26.05

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-12 Engine Fire and

Overheat Detection


Detection Loop

B on the

Engine 1

26-12-03A C 1 0 May be inoperative provided that the engine fire test is

made before each flight.


Detection Loop

B on the

Engine 2

26-12-04A C 1 0 One may be inoperative provided that the engine fire test

is made before each flight.

26-12-05 FIRE light on the

ENG MASTER

Panel


26-13 APU Fire and

Overheat Detection

26-13-01 APU Fire

Detection

Loop A

26-13-01A C 1 0 One may be inoperative provided that:

1) The associated detection loop B is operative and,

2) The APU fire test is made before each APU start, and3) During APU operations on ground, APU condition is

continuously monitored in the cockpit.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-13 APU Fire and

Overheat

Detection

26-13-01 APU Fire

Detection

Loop A

26-13-01B C 1 0 (M) One may be inoperative provided that the APU is

deactivated.


26-13-02 APU Fire

Detection

Loop B

26-13-02A C 1 0 One may be inoperative provided that the APU fire test is

made before each APU start.

26-13-02B C 1 0 (M) One may be inoperative provided that the APU is

deactivated.


26-15 Avionics

Compartment

Smoke Detection

26-15-01 Avionics Smoke

Detection

System

26-15-01A A 1 0 (O)(FD) May be inoperative.



Disregard the BLOWER pb-sw FAULT light and the CAB

FANS pb-sw FAULT light illuminated on the

VENTILATION overhead panel.

IN FLIGHT

In the case of an electrical smoke:

Apply the AVNCS SMOKE emergency procedure.Refer to the QRH/ABN-26-FIRE PROTECTION.

12 FEB 12MEL

A320/321MEL/CDL 01.26.07

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION


Smoke Detection

26-16-01 Smoke Detector

in the FWD

Cargo

Compartment

(A320)

Note:

i. The cargo smoke detection function is part

of the CIDS Smoke Detection Function

(CIDS-SDF).

Refer to Item 23-73-10-01 Smoke DetectionFunction (CIDS-SDF)

ii. Failure of a single detector in the cavity is

indicated by a MAINTENANCE message on

the STATUS SD page.


MAINTENANCE Message

iii. Depending on applicable regulation, smoke

detection system may be required for

dispatch.

26-16-01A Empty FWD

cargocompartment

C 2 0 (O)(FD) Both detectors in the cavity may be inoperative provided

that the FWD cargo compartment is empty.


Refer to item 26-16-01D for operating procedure.

26-16-01D Check of liner

integrity

B 2 0 (O)(FD) Both detectors in the cavity may be inoperative provided

procedure are established and used to verify associated

cargo compartment remains empty or contains only empty

cargo containers, cargo handling equipment, pallets,

ballast (ballast may be loaded in ULD's).


Ramp Load Control Supervisor to physically check and

confirm to the flight crew that cargo compartment(s) are

either empty or only contain empty cargo containers,

pallets, cargo restraint components



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-16 Cargo

Compartment

Smoke Detection


in the FWD

Cargo

Compartment

(A321)

Note:

i. The cargo smoke detection function

is part of the CIDS Smoke Detection

Function (CIDS-SDF).

Refer to Item 23-73-10-01 SmokeDetection Function (CIDS-SDF)

ii. Failure of a single detector in the

cavity is indicated by a

MAINTENANCE message on the

STATUS SD page.

Refer to Item 26-00-01

SDCU/SMOKE MAINTENANCE

Message

26-16-01A B 4 0 (O)(FD) Both detectors in one or both cavities may be inoperative

provided that the FWD cargo compartment is empty or

does not contain flammable or combustible materials.






01 MAY 12MEL

A320/321MEL/CDL 01.26.09

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION


Smoke Detection


in the AFT and

the BULK Cargo

Compartments

(A321)

Note:

i. The cargo smoke detection function is part

of the CIDS Smoke Detection Function

(CIDS-SDF).

Refer to Item 23-73-10-01 Smoke DetectionFunction (CIDS-SDF)

ii. Failure of a single detector in the cavity is

indicated by a MAINTENANCE message on

the STATUS SD page.


MAINTENANCE Message

26-16-02A B 6 0 (O)(FD) Both detectors in one or more cavities may be inoperative

provided that the AFT and the BULK cargo compartments

are empty or do not contain flammable or combustible

materials.








MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-16 Cargo

Compartment

Smoke Detection


in the AFT and

the BULK Cargo

Compartments

(A320)

26-16-02C C 4 2 (O) Both detectors in one or both cavities may be inoperative

provided that the AFT cargo ventilation is closed.



Life animal not allowed to be on associated cargo.


AFT ISOL VALVE pb-sw . . . . . . . . . . . . . . . . . . . . OFF

26-16-02E Check of liner

integrity

B 4 0 (O) Both detectors in one or both cavities may be inoperative

provided that:

1) The liner integrity in the AFT and the BULK cargocompartments is checked before each flight, and

2) The AFT cargo ventilation is closed.


Refer to MEL item 26-16-02C

12 FEB 12MEL

A320/321MEL/CDL 01.26.11

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-17 Lavatory Smoke

Detection

26-17-01 Lavatory Smoke

Detection

System

Note:

The lavatory smoke detection function is

part of CIDS Smoke Detection Function

(CIDS-SDF).

Refer to Item 23-73-10-01 Smoke

Detection Function (CIDS-SDF)


lavatory fire

extinguishing

system

operative

C 3 1 (O) One or two may be inoperative provided that:

1) The associated lavatory fire extinguishing system isoperative, and

2) A procedure is used to periodically check absence of smoke in the associated lavatory.


PIC request the cabin purser to Ensure that the affected

lavatory is inspected and checked by crewmembers

periodically during flight.


lavatory not

used

C 3 2 (O)(FD) One may be inoperative provided that:

1) The associated lavatory waste receptacle is empty,and

2) The associated lavatory door is locked closed andplacarded inoperative, and

3) The lavatory is not used for storage or for any other purpose, and

4) A procedure is used to periodically check the absenceof smoke in the associated lavatory.

5) Refer to the NOTE in Operating Procedure




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-17 Lavatory Smoke

Detection

26-17-01 Lavatory Smoke

Detection

System


lavatory not

used (cont’d)


The associated lavatory is periodacally checked for the

absence of smoke by crewmembers.

NOTE:

In case foreword lavatory placarded

extra pilot should be assigned to

operate the flight as a safety pilot to

relieve the pilot when leaving the cockpit

for personal reasons.

26-22 APU Fire

Extinguishing

26-22-01 APU Automatic

Fire

Extinguishing

Control on

Ground

26-22-01A APU operations

on ground

monitored

C 1 0 May be inoperative provided that the APU condition is

continuously monitored in the cockpit during APU

operations on ground .

12 FEB 12MEL

A320/321MEL/CDL 01.26.13

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-22 APU Fire

Extinguishing

26-22-02 APU Fire

Extinguisher

Overpressure

Indication (Red

Disc)

26-22-02A APU Fire

extinguisher

bottle pressure

switch operative

C 1 0 (M) May be damaged or missing provided that the APU fire

extinguisher bottle pressure switch is checked operative

before the fist flight of each day.


Refer to AMM 26-22-00-040-007

26-22-02B APU

deactivated





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-22 APU Fire

Extinguishing

26-22-03 Squib of the

APU Fire

Extinguisher

Bottle

26-22-03A One

inoperative

C 2 1 (M) One may be inoperative provided that the remaining squib

is checked operative before the fist flight of each day.


Refer to AMM 26-22-00-040-008

26-22-03B Both

inoperative

C 2 0 (M) Both m ay b e inoperative p rovided t hat t he A PU i s

deactivated.


26-22-04 APU Fire

Extinguisher

Bottle

26-22-04A C 1 0 (M) May be inoperative provided that the APU is deactivated.


12 FEB 12MEL

A320/321MEL/CDL 01.26.15

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-22 APU Fire

Extinguishing

26-22-05 APU AUTO

EXTING TEST

pb-sw on the

Maintenance

Panel

26-22-05A C 1 0 May be inoperative provided that the APU automatic fire

extinguishing control on ground is considered inoperative.

Refer to Item 26-22-01 APU Automatic Fire Extinguishing

Control on Ground

26-22-06 APU FIRE light

on the External

Power Panel

26-22-06A APU Automatic

fire

extinguishing

control on

ground

operative

C 1 0 (M) May be inoperative provided that the APU automatic fire

extinguishing control on ground is checked operative.


Refer to AMM 26-22-00-040-010

26-22-06B APU Automatic

fire

extinguishing

control on

ground

considered

inoperative

C 1 0 May be inoperative provided that the APU automatic fire


Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-22 APU Fire

Extinguishing

26-22-07 APU SHUT OFF

pb on the

External Power

Panel

26-22-07A APU Automatic

fire

extinguishing

control on

ground

operative

C 1 0 (M) May be inoperative provided that the APU automatic fire

extinguishing control on ground is checked operative.


Refer to AMM 26-22-00-040-011

26-22-07B APU Automatic

fire

extinguishing

control on

ground

considered

inoperative

C 1 0 May be inoperative provided that the APU automatic fire


Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground

26-23 Cargo

Compartment Fire

Extinguishing

26-23-01 Cargo Agent

Bottle

Note:

The cargo smoke detection function is

part of CIDS Smoke Detection Function

(CIDS-SDF).

Refer to Item 23-73-10-01 Smoke

Detection Function (CIDS-SDF)


12 FEB 12MEL

A320/321MEL/CDL 01.26.17

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION


Fire Extinguishing

26-23-01 Cargo Agent

Bottle (cont’d)

26-23-01A No flammable

or combustible

materials

C 1 0 (O)(FD) May be inoperative provided that the cargo compartments

are empty or do not contain flammable or combustible

materials.





pallets, cargo restraint components.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-23 Cargo

Compartment Fire

Extinguishing

26-23-02 Squib of the

Cargo Bottle 1

26-23-02A No flammable

or combustible

materials

C 2 0 (O)(FD) O ne or both may be inoperative provided that the

associated cargo compartment is empty or does not





either empty or only contain empty carfo containers,

pallets, cargo restraint components.

26-24-01 Portable Fire

Extinguisher

26-24-01A C 4 3 One may be inoperative in the cabin or missing provided:

1) Inoperative fire extinguisher is tagged inoperative,removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit, and

2 ) Required distribution is maintained.

Note:

The fire extnguisher located in the

cockpit must always be operative.

12 FEB 12MEL

A320/321MEL/CDL 01.26.19

FIRE PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


26 FIRE PROTECTION

26-24 Portable Fire

Extinguisher

26-25 Lavatory Fire

Extinguishing

26-25-01 Lavatory Waste

Bin Fire

Extinguishing

System

26-25-01A C 3 0 One or more may be inoperative provided associated

lavatory smoke detection system is operative.

26-25-01B C 3 2 (O)(M)

(FD)

One may be inoperative provided:

1) Lavatory waste receptacle is emty,

2) Lavatory door is locked closed and placarded "

"INOPERATVIE DONT ENTER", and

3) lavatory is used only by crewmembers.

4) Refer to the NOTE in Operating Procedure.

NOTE:

These provisos are not intented to

prohibit lavatory use or inspection by

crewmembers.

OPERATING PROCEDUERS

Ensure that the affected lavatory is kept locked and is not

entered except for inspection by crewmembers.

NOTE:

In case foreword lavatory placarded extra pilot should be

assigned to operate the flight as a safety pilot to relieve

the pilot when leaving the cockpit for personal reasons.

* * *



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-00 MAINTENANCE

Messages on the

STATUS SD page

27-00-01 F/CTL

MAINTENANCE

Message

27-00-01A C 1 - F/CTL MAINTENANCE message may be displayed on the

STATUS SD page.

27-00-02 SFCS

MAINTENANCE

Message

27-00-02A C 1 - SFCS MAINTENANCE message may be displayed on the

STATUS SD page.


27-01-01 FLT CTL

Overhead Panel

27-01-01-01 ELAC pb-sw

FAULT light


27-01-01-02 ELAC pb-sw

OFF light


27-01-01-03 SEC pb-sw

FAULT light




SEQUENCE


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.27.01

FLIGHT CONTROLS

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


27-01-01 FLT CTL

Overhead Panel

27-01-01-04 SEC pb-sw OFF

light



pages

27-07-01 Aileron Actuator

Indication on the

F/CTL SD page


27-07-02 Aileron Position

Indication on the

F/CTL SD page

27-07-02A C 2 1 (O)(FD) One may be inoperative provided that the deflection of the

affected aileron through each servo-control is visually




Note:

If the Yellow Electric Pump is not

available:

- Pressurize the Yellow Hydraulic System

with:- A Ground cart, or with

- The Yellow Engine 2 Pump with

the Engine 2 running.


01.27.02FLIGHT CONTROLS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages


Indication on the

F/CTL SD page


- Replace any action on the YELLOW

ELEC PUMP pb-sw by a similar action on the Ground Cart or on the

YELLOW ENG 2 PUMP pb-sw in the

following procedure.

Check of the aileron control through the ELACs:

Put the aircraft in the test configuration:

- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON

- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO

- BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON

- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

Check of the aileron control through the ELAC 1:

- Move the CAPT stick from right stop to left stop.

- Visually check the full travel of the ailerons.

CAUTION

If the expected aileron movement does

not occur, do not attempt any reset.

Contact the maintenance.


12 FEB 12MEL

A320/321MEL/CDL 01.27.03

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages


Indication on the

F/CTL SD page


Check of the aileron control through the ELAC 2:

- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF

- Move the CAPT stick from right stop to left stop,then from forward stop to aft stop.

- Visually check the full travel of the ailerons.

CAUTION

If the expected aileron movement does



Return to normal configuration:- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off

- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . Off

- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On

27-07-03 Elevator

Actuator

Indication on the

F/CTL SD page




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-04 Elevator

Position

Indication on the

F/CTL SD page

27-07-04A C 2 1 (O) One may be inoperative provided that the deflection of the

affected elevator is visually checked before each flight.



Note:


available:

- Pressurize the Yellow Hydraulic

System with:

- A Ground cart, or with


the Engine 2 running.- Replace any action on the YELLOW

ELEC PUMP pb-sw by a similar

action on the Ground Cart or on the



Check of the elevator control:


- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO




12 FEB 12MEL

A320/321MEL/CDL 01.27.05

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-04 Elevator

Position

Indication on the

F/CTL SD page

27-07-04A (Cont’d) OPERATING PROCEDURES (Cont’d)

- Establish communication with the ground crew.

- Move the CAPT or the F/O stick to the maximumnose down position.

- Visually check that both elevators move down.

- Move the CAPT or the F/O stick to the maximumnose up position.

- Visually check that both elevators move up.

- Move the CAPT or the F/O stick to the neutralposition.

- Visually check that both elevators go back to the

neutral position.- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off

- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . Off

27-07-05 Pitch Trim

Position

Indication on the

F/CTL SD page

27-07-05A C 1 0 (O) May be inoperative provided that the pitch trim handwheel

and the stabilizer are visually checked to synchronously

operate before each flight.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-05 Pitch Trim

Position

Indication on the

F/CTL SD page



Note:


available:


System with:









Check of the stabilizer control:



- Move the pitch trim handwheel to the full DNposition.

- Visually check that the stabilizer moves to the fulldown position.

- Move the pitch trim handwheel to the full UPposition.

- Visually check that the stabilizer moves to the fullup position.

- Move the pitch trim handwheel to the requiredposition.

- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off

12 FEB 12MEL

A320/321MEL/CDL 01.27.07

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-06 Rudder Position

Indication on the

F/CTL SD page

27-07-06A B 1 0 (O) May be inoperative provided that the deflection of the

rudder is visually checked before each flight.



Note:


available:


with:




- Replace any action on the YELLOW ELECPUMP pb-sw by a similar action on the

Ground Cart or on the YELLOW ENG 2

PUMP pb-sw in the following procedure.

Check of the rudder control:

- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON


- On the CAPT or the F/O side, apply left rudder.

- Visually check that the rudder moves to the left.

- On the CAPT or the F/O side, apply right rudder.- Visually check that the rudder moves to the right.

- On the CAPT or the F/O side, release the pedals.

- Visually check that the rudder moves to the neutralposition.

- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-07 Rudder Trim

Position

Indication on the

F/CTL SD page

27-07-07A Rudder trim

position

indication

operative on the

center pedestal

C 1 0 May be inoperative provided that the rudder trim position

indication is operative on the center pedestal .

27-07-07B Rudder position

checked at zero

C 1 0 May be inoperative provided that the rudder position is

checked at zero on the F/CTL SD page before takeoff.

27-07-08 Rudder Travel

Limiter Position

Indication on the

F/CTL SD page


27-07-09 ELAC Indication

on the F/CTL SD

page


27-07-10 SEC Indication

on the F/CTL SD

page


12 FEB 12MEL

A320/321MEL/CDL 01.27.09

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-11 Spoilers/

Speedbrakes

Indication on

the F/CTL SD

page

27-07-11A C 10 0 (O) One or more may be inoperative provided that the

deflection of the affected surface is visually checked

before each flight.



Note:


available:


with:

- A Ground cart, or with- The Yellow Engine 2 Pump with


- Replace any action on the YELLOW ELEC

PUMP pb-sw by a similar action on the



- If surface 1 indication is inoperative:

CAUTION

The aircraft must be stopped during the

check.

- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . ON

- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

- SPEEDBRAKES lever . . . . . . . . . . . . . . . . . . FULL

- Visually check that surface 1 slightly extends

(approximately 6°).




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-11 Spoilers/

Speedbrakes

Indication on

the F/CTL SD

page


- YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . Off



- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON

- Move the stick from left stop to right stop.

- Visually check the correct movement of surface 3.

- BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off

- If surface 2, 4, or 5 indication is inoperative:


- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

- Move the stick from left stop to right stop andvisually check the correct movement of surfaces 2,4 and 5.


27-07-12 Spoilers/

Speedbrakes

Indication on the

WHEEL SD page

27-07-12A C 10 0 (O) One or more may be inoperative provided that thedeflection of the affected surface is visually checked

before each flight.


12 FEB 12MEL

A320/321MEL/CDL 01.27.11

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-12 Spoilers/

Speedbrakes

Indication on the

WHEEL SD page



Note:


available:


with:





PUMP pb-sw by a similar action on theGround Cart or on the YELLOW ENG 2



CAUTION

The aircraft must be stopped during the

check.


- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

- SPEEDBRAKES lever . . . . . . . . . . . . . . . . . . FULL

- Visually check that surface 1 slightly extends

(approximately 6°).

- YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


pages

27-07-12 Spoilers/

Speedbrakes

Indication on the

WHEEL SD page





- Move the stick from left stop to right stop.

- Visually check the correct movement of surface 3.


- If surface 2, 4, or 5 indication is inoperative:


- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

- Move the stick from left stop to right stop andvisually check the correct movement of surfaces 2,4 and 5.



EWD

27-08-01 Flap Position

Indication on the

EWD


27-08-02 Slat Position

Indication on the

EWD


12 FEB 12MEL

A320/321MEL/CDL 01.27.13

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-14 Aileron and Hydraulic

Actuation

27-14-01 Left Aileron Blue

Servo-Control

(Controlled by

ELAC 1)

27-14-01A A 1 0 (O)(M) May be inoperative provided that:

1) It is electrically disconnected, and

2) It remains mechanically connected and hydraulicallysupplied (damping function is not affected), and

3) The left aileron green servo-control (controlled byELAC 2) is operative, and

4) The right aileron blue servo-control (controlled byELAC 2) is operative, and

5) All roll spoilers are operative, and

6) The TR 1 and TR 2 are operative, and

7) The DC TIE contactor 1PC1 is checked closed, and

8) Repaire with in three flight days.



Check that DC TIE contactor 1 is closed:


- On the ELEC SD page, check the link between theDC BUS 1 and the DC BAT BUS.


Refer to AMM 27-14-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-14 Aileron and

Hydraulic

Actuation

27-14-02 Left Aileron

Green Servo-

Control

(Controlled by

ELAC 2)




3) All roll spoilers are operative.


Refer to AMM 27-14-00-040-001

27-14-03 Right Aileron

Green Servo-

Control

(Controlled by

ELAC 1)

27-14-03A A 1 0 (O)(M) May be inoperative provided that:



3) The right aileron blue servo-control (controlled byELAC 2) is operative, and

4) The left aileron green servo-control (controlled by

ELAC 2) is operative, and

5) All roll spoilers are operative, and



8) Repaire with in three flight days.


12 FEB 12MEL

A320/321MEL/CDL 01.27.15

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-14 Aileron and Hydraulic

Actuation


Green Servo-

Control

(Controlled by

ELAC 1)



Check that DC TIE contactor 1 is closed:


- On the ELEC SD page, check the link between the DCBUS 1 and the DC BAT BUS.


Refer to AMM 27-14-00-040-001


Blue Servo-

Control

(Controlled by

ELAC 2)




3) All roll spoilers are operative.


Refer to AMM 27-14-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-21 Rudder

Mechanical

Control

27-21-01 Rudder Pedal

Adjustment

System

27-21-01A C 2 1 (O) One may be inoperative provided that:

1) The rudder pedals can be secured in a position whichmeets individual pilot requirements, and

2) The full and unrestricted movement of the rudder pedals and brake pedals deflection is possible at bothpilot stations.



Simultaneously apply loads on both pedals (in rudder

control movement direction) to make sure that the secured

position is reached. For that purpose, the effort shall be

equivalent to a full rudder deflection.

27-22 Rudder Trim

Actuation


System

27-22-01A Rudder trim

system 1

inoperative

C 2 1 (O) Rudder Trim System 1 may be inoperative.




27-22-01B Rudder trim

system 2

inoperative

C 2 1 (O) Rudder Trim System 2 may be inoperative.


Refer to MEL item 27-22-01A

12 FEB 12MEL

A320/321MEL/CDL 01.27.17

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-22 Rudder Trim

Actuation

27-22-02 Manual Rudder

Trim Reset

Function

27-22-02A C 1 0 May be inoperative provided that one rudder trim position

indication is operative.


Position

Indication on the

Center Pedestal


27-23 Artificial feel and

rudder travel limiting

actuation

27-23-01 Rudder Travel

Limiter System(Including

Rudder and

Pedals Travel

Limiter Units)


27-34 Elevator and

Hydraulic Actuation

27-34-01 Elevator Servo-

Control

27-34-01A 4 4 All must be operative.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-34 Elevator and

Hydraulic

Actuation

27-34-02 Elevator Servo-

Control Position

Transducer

27-34-02A C 4 2 (M) One transducer per servo-control must be operative.


Refer to AMM 27-34-00-040-001

27-40 Trimmable

Horizontal

Stabilizer (THS)

27-40-01 Stabilizer

Mechanical

Control


27-40-02 Stabilizer

Actuator Electric

Motor

27-40-02A Electric motor 3

inoperative

C 3 2 The stabilizer actuator electrical motor 3 may be

inoperative.

27-40-02-B Electric motor 2

inoperative

C 3 2 The stabilizer actuator electric motor 2 may be inoperative

provided that ELAC 1 pitch channel is considered

inoperative.

Refer to Item 27-93-01 ELAC 1

12 FEB 12MEL

A320/321MEL/CDL 01.27.19

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27-51 Flaps Electrical

Control and

Monitoring

27-51-01 SFCC Flap

Channel

27-51-01A B 2 1 (O)(M) SFCC 2 flap channel may be inoperative provided that:

1) It is deactivated, and

2) The slats and flaps are checked operative on SFCC 1,and

3) The SFCC 1 flap WTB is checked operative beforeeach flight, and

4) All ELACs, SECs, LGCIUs, RAs, FACs and ADIRS areoperative, and

5) The minimum idle on ground is considered inoperative.

Refer to Item 73-20-05 Minimum Idle on Ground


GENERAL INFORMATION

ENG 2 APPR IDLE ONLY message is displayed onthe STATUS SD page.

FLAPS SLOW message is displayed on the STATUSSD page.


Disregard and clear the F/CTL FLAP SYS 2 FAULTalert displayed on the EWD.


Refer to AMM 27-51-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-51 Flaps Electrical

Control and

Monitoring

27-51-02 SFCC Slat

Channel

27-51-02A B 2 1 (O)(M) SFCC 2 slap channel may be inoperative provided that:


2) The slats and flaps are checked operative on SFCC 1,and

3) The SFCC 1 slat WTB is checked operative beforeeach flight, and

4) All ELACs, SECs, LGCIUs, RAs, FACs and ADIRS areoperative, and

5) Takeoff is not performed in CONF 1+F.


GENERAL INFORMATION

SLATS SLOW message is displayed on the STATUS

SD page.


Disregard and clear the F/CTL SLAT SYS 2 FAULTalert displayed on the EWD.

MAINTENANCE PROCEDUR

Refer to AMM 27-51-00-040-005

27-51-03 Flap Wing Tip

Brakes Solenoid

27-51-03A B 4 2 (M) One or two solenoids associated with the SFCC 2 may beinoperative provided that the SFCC 1 flap WTB is checked

operative before each flight.


Refer to AMM 27-51-00-040-004

12 FEB 12MEL

A320/321MEL/CDL 01.27.21

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-54 Flaps Hydraulic

Actuation and Power

Transmission

27-54-01 Flap Hydraulic

Motor

27-54-01A Green motor

inoperative

C 2 1 Green motor may be inoperative.

27-54-01B Yellow motor

inoperative

C 2 1 Yellow motor may be inoperative provided that the blue

slat motor is operative.

27-54-02 Flap PCU Valve

Block

27-54-02A B 2 1 The valve block associated with SFCC 2 may be

inoperative provided that the SFCC 2 flap channel is


Refer to Item 27-51-01 SFCC Flap Channel

27-54-03 Flap Pressure-

Off Brake




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-64 Spoiler Hydraulic

Actuation

27-64-01 Spoiler 5

27-64-01A C 2 0 (O)(M) The pair of spoilers 5 may be inoperative provided that:

1) The affected spoiler is deactivated in the retractedposition, and

2) The pairs of spoilers 1, 2, 3, and 4 are operative.


AFTER ENGINE START

On the HYD SD page, check the absence of amber data.

Note:

No performance penalty applies when

the pair of spoilers 5 is inoperative.


Refer to AMM 27-64-00-040-001

27-64-02 Spoiler 1 or 3

27-64-02A C 4 2 (O)(M)

(FD)

One pair of spoilers 1 or 3 may be inoperative provided

that:


2) The pairs of spoilers 2, 4, and 5 are operative, and

3) The Flight Manual performance penalties are applied.



For performance calculations request Modified Tailored

Takeoff and Landing charts (MTTL) from FPE through

Flight Dispatch.


30 JUN 12MEL

A320/321MEL/CDL 01.27.23

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Actuation

27-64-02 Spoiler 1 or 3


Landing performance computation:

Increase the landing distances by 10 %.

AFTER ENGINE START


FOR TAKEOFF

Performed the takeoff using full thrust (TOGA).


Refer to AMM 27-64-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Actuation

27-64-03 Spoiler 2 or 4

27-64-03A C 4 2 (O)(M)(FD)

One pair of spoilers 2 or 4 may be inoperative in theretracted position provided that:



3) The SFCC 2 flap channel is operative, and




For performance penalties, Refer to OperatingProcedures 27-64-02A Spoiler 1 or 3

AFTER ENGINE START



Refer to AMM 27-64-00-040-001

30 JUN 12MEL

A320/321MEL/CDL 01.27.25

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Actuation

27-64-04 Spoilers 1 and 2

27-64-04A B 4 0 (O)(M)

(FD)

The pairs of spoilers 1 and 2 may be inoperative in the

retracted position provided that:

1) The affected spoilers are deactivated in the retractedposition, and




OPERATING PROCEDURES (A321)


For performance calculations request ModifiedTailored Takeoff and Landing charts (MTTL) from FPEthrough Flight Dispatch.




- SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Actuation


27-64-04A (cont’d) OPERATING PROCEDURES (A321) cont’d

FOR TAKEOFF


IN FLIGHT

- In the case of further failure of SEC 1 and SEC 2:

- Autoland is not permitted.

- Disengage the AP at 500 ft RA before landing in

direct law. As soon as the AP is disengaged whenthe three SECs are failed, it cannot be engagedagain.

- Maximum landing capability is CAT I


30 JUN 12MEL

A320/321MEL/CDL 01.27.27

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Actuation


27-64-04A (cont’d) OPERATING PROCEDURES (A320)


For performance calculations request ModifiedTailored Takeoff and Landing charts (MTTL) from FPEthrough Flight Dispatch .




- SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B

· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull

FOR TAKEOFF


IN FLIGHT

- In the case of further failure of SEC 1 and SEC 2:

- Autoland is not permitted.

- Disengage the AP at 500 ft RA before landing indirect law. As soon as the AP is disengaged whenthe three SECs are failed, it cannot be engagedagain.

- Maximum landing capability is CAT I


Refer to AMM 27-64-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27FLIGHT CONTROLS


Actuation


27-64-05A C 4 0 (O)(M)

(FD)

The pairs of spoilers 3 and 4 may be inoperative in the

retracted position provided that:

1) The affected spoilers are deactivated in the retractedposition, and








For performance penalties Refer to OperatingProcedures 27-64-04A Spoilers 1 and 2


Check that the DC TIE contactor 1 is closed:



IN FLIGHT

Do not use the speedbrakes.


Refer to AMM 27-64-00-040-001

30 JUN 12MEL

A320/321MEL/CDL 01.27.29

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


.27 FLIGHT CONTROLS

27-81 Slats Electrical

Control and

Monitoring

27-81-01 Slat Wing Tip

Brakes

Solenoids

27-81-01A C 4 2 (M) One or two solenoids associated with the SFCC 2 may be

inoperative provided that the SFCC 1 slat WTB is checked



Refer to AMM 27-81-00-040-001

27-84 Slats Hydraulic

Actuation and Power

Transmission

27-84-01 Slats Hydraulic

Motor


27-84-02 Slat PCU Valve

Block

27-84-02A C 2 1 The valve block associated with SFCC 2 may be

inoperative provided that the SFCC 2 slat channel is


Refer to MEL Item 27-51-02 SFCC Slat Channel

27-84-03 Slat Pressure-

Off Brake




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-92 Electrical Flight

Control System

(EFCS) Control

Inputs and Power

Supply

27-92-01 Speedbrake

Control System

27-92-01B Speedbrake 2

or speedbrakes

3 and 4

inoperative

B 1 1 (O)(FD) Speedbrake 2 or speedbrakes 3 and 4 may be inoperative

provided that the Flight Manual performance penalties

associated with one or two pairs of spoilers inoperative are

applied.



- If speedbrake n° 2 is inoperative: Apply performance penalties associated with the pair of spoilers 2 inoperative.Refer to Operating Procedures 27-64-03A Spoiler 2 or 4

- If speedbrakes n° 3 and n° 4 are inoperative: Apply performance penalties associated with two pairsof spoilers inoperative.Refer to Operating Procedures 27-64-04A Spoilers 1and 2

IN FLIGHT

- If speedbrakes n° 3 and n° 4 are inoperative:Do not use the speedbrakes.

30 JUN 12MEL

A320/321MEL/CDL 01.27.31

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Control System

(EFCS) Control Inputs

and Power Supply

27-92-02 Ground Spoiler

Control System

27-92-02A Ground spoiler

control system

inoperative

A 1 0 (O)(FD) May be inoperative provided that:

1) Both thrust reversers are not taken into account for performance computation, and

2) The autobrake function is not used, and

3) The Flight Manual performance penalties are applied,and

4) Repair must be made within three flight legs.


GENERAL INFORMATION

The autobrake function is not available.

Refer to Operating Procedures 32-42-05A AUTO/BRK Function

CAUTION

One or both thrust reversers may not

deploy at landing. Consequently, for

performance determination, do not take

into account the credit of the thrust

reversers.


For performance calculations request ModifiedTailored Takeoff and Landing charts (MTTL) from FPE

through Flight Dispatch.



FOR TAKEOFF





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Control System

(EFCS) Control

Inputs and Power

Supply


Control System

27-92-02A (Cont’d) OPERATING PROCEDURES (A320)

GENERAL INFORMATION

The autobrake function is not available.

Refer to Operating Procedures 32-42-05A AUTO/BRK Function

CAUTION

One or both thrust reversers may not

deploy at landing. Consequently, for

performance determination, do not takeinto account the credit of the thrust

reversers.


For performance calculations request ModifiedTailored Takeoff and Landing charts (MTTL) from FPEthrough Flight Dispatch .



FOR TAKEOFF


30 JUN 12MEL

A320/321MEL/CDL 01.27.33

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Control System

(EFCS) Control Inputs

and Power Supply


Control System

27-92-02B Spoilers 5

inoperative

C 1 1 (O) The pair of spoilers 5 may be inoperative.



For performance penalties, Refer to Operating Procedures

27-64-01A Spoiler 5

27-92-02C Spoilers 1 and

2, or spoilers 3

and 4

inoperative

C 1 1 (O) The pairs of spoilers 1 and 2 or the pairs of spoilers 3 and

4 may be inoperative provided that the Flight Manual

performance penalties are applied.



- If the pairs of spoilers 1 and 2 are inoperative:

For performance penalties, Refer to OperatingProcedures 27-64-04A Spoilers 1 and 2

- If the pairs of spoilers 3 and 4 are inoperative:


27-92-03 SIDESTICK

PRIORITY light




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


Control System

(EFCS) Control

Inputs and Power

Supply

27-92-04 Sidestick Dual

Input Visual

Warnings


27-92-05 Sidestick Dual

Input Aural

Warning


27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1

27-93-01A B 1 0 (O)(M)

(FD)

ELAC 1 or any ELAC 1 function may be inoperative

provided that:

1) All SECs, SFCCs, LGCIUs, RAs, ADIRS and FACsare operative, and

2) The pairs of spoilers 2, 3, 4, and 5 are operative, and

3) The TR 1 and the TR 2 are operative, and

4) Both accelerometers associated with the ELAC 2 arechecked operative before each flight, and

5) All sidesticks transducers associated with the ELAC 2

and the three SECs are checked operative beforeeach flight, and

6) The DC TIE contactor 1PC1 is checked closed, beforeeach flight, and

7) The elevators and roll spoilers control is checkedoperative through the SECs before each flight.


30 JUN 12MEL

A320/321MEL/CDL 01.27.35

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1

27-93-01A (Cont’d) Note:

F/O take-over pb cannot disengage

AP1.



If the AP 1 is engaged for landing: Maximum landingcapability is CAT I.

If the AP 2 is engaged for landing: Landing capabilityis CAT II.


Note:


available:


with:








- If the F/CTL ELAC 1 FAULT alert is displayed on the

EWD:




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1


Note:

i. After application of the maintenanceprocedure, the following ECAM

alerts remain displayed on the EWD:

- C/B TRIPPED R ELEC BAY

alert , and

- C/B TRIPPED ON OVHD PNL

alert, and

- F/CTL ELAC 1 FAULT alert.

ii. After first engine start, the F/CTL

ALTN LAW alert may be spuriously

displayed. It normally disappears

after second engine start.

Check of the elevator and the roll spoilers control throughthe SECs:



Note:


available, pressurize the Yellow

Hydraulic System with a Ground Cart or

with the Yellow Engine 2 Pump with the

Engine 2 running.

- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO




30 JUN 12MEL

A320/321MEL/CDL 01.27.37

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1


- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On

- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On

- SEC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- SEC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- Wait 5 s

Check of the elevator control through the SEC 1 and the

spoilers control through the secretary 1 and the SEC 3:

- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off

- Wait for hydraulic circuit depressurization.

- On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.

- Wait 5 s

- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON

- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.

- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.

- Move the F/O stick from right stop to left stop, thenfrom forward stop to aft stop.





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1


CAUTION

If an expected spoiler or elevator movement does not occur, do not

attempt any reset.


Check of the elevator control through the SEC 2 and of the

spoilers control through the SEC 2 and the SEC 3:

- ELAC 1 & 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · On

- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Wait 5 s

- YELLOW ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · Off

- Wait for hydraulic circuits depressurization.

- On the F/CTL SD page, check that the yellow and thegreen elevator actuators symbols become amber.

- Wait 5 s


- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF


- On the F/CTL SD page, check the correct movementof the pairs of spoilers 2 and 5 and the full travel of both elevators.




30 JUN 12MEL

A320/321MEL/CDL 01.27.39

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1


CAUTION

If an expected spoiler or elevator movement does not occur, do not

attempt any reset.


Return to normal configuration:

- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · OFF

- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · OFF

- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On




- If the F/CTL ELAC 1 PITCH FAULT alert is displayedon the EWD:

Note:

After first engine start:

- The F/CTL ALTN LAW alert may bespuriously displayed on the EWD. It

normally disappears after few seconds when

ELAC 2 auto test is accomplished.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1


Check of the elevator and the roll spoilers control through

the SECs:



- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

- BLUE ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · AUTO

- BLUE PUMP OVRD pb · · · · · · · · · · · · · · · · · · · · · · ON

- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On- SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Wait 5 s






- Wait 5 sincerely- BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON

- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF


30 JUN 12MEL

A320/321MEL/CDL 01.27.41

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1






CAUTION

If an expected spoiler or elevator

movement does not occur, do not

attempt any reset.




- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Wait 5 s




- Wait 5 s


- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1


- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF





CAUTIONIf an expected spoiler or elevator


attempt any reset.





- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On


30 JUN 12MEL

A320/321MEL/CDL 01.27.43

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-01 ELAC 1





BEFORE ENGINE START

- AP 1 pb · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- CAPT take-over pb · · · · · · · · · · · · · · · · · · · · · · · Press

- Check that the AP OFF message is displayed on theEWD.

Note:

Due to the fact that the ELAC 1 is not

electrically supplied, the F/O take-over

pb cannot disengage the AP 1.

IN APPROACH

- If the AP 1 is used for the approach:

The captain must be the PF.


Refer to AMM 27-93-00-040-001

27-93-02 ELAC 2




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-93 ELAC System

(Elevator Aileron

Computer)

27-93-03 Pitch Normal

Law


27-94 SEC System

(Spoiler and

Elevator

Computer)

27-94-01 SEC 1

27-94-01A B 1 0 (O)(M)

(FD)

May be inoperative provided that:


2) The SEC 2 and the SEC 3 are operative, and

3) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRSare operative, and


5) All aileron servo-controls associated with the operativeSECs are operative, and


7) The sidestick transducers associated with the ELACsand the operative SECs are checked operative beforeeach flight, and

8) The DC TIE contactor 1PC1 is checked closed, beforeeach flight, and

9) The elevators control through the SEC 2 and theELACs and the roll spoilers control through the

operative SECs are checked operative before eachflight, and

10) The Flight Manual performance penalties for the pairsof spoilers 3 and 4 inoperative are applied.


30 JUN 12MEL

A320/321MEL/CDL 01.27.45

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-94 SEC System (Spoiler

and Elevator

Computer)

27-94-01 SEC 1





Note:


available:


with:








Note:

After application of the maintenance

procedure, the C/B TRIPPED R ELEC

BAY and the C/B TRIPPED ON OVHD

PNL alerts are displayed on the EWD.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-94 SEC System

(Spoiler and

Elevator

Computer)

27-94-01 SEC 1


Check of the elevator control through the operative

computers:



- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO



- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- SEC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- Wait 5 s

Check of the elevator control through the ELAC 1:




- Wait 5 s


- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- Move the CAPT stick from forward stop to aft stop.

- On the F/CTL SD page, check the full travel of bothelevators.


30 JUN 12MEL

A320/321MEL/CDL 01.27.47

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


and Elevator

Computer)

27-94-01 SEC 1


CAUTION

If an expected elevator movement doesnot occur, do not attempt any reset.


Check of the elevator control through the SEC 2:

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Wait 5 s




- Wait 5 s


- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.Each stop must be applied during 3 s

- On the F/CTL SD page, check the correct movement

of the pairs of spoilers 2 and 5 and the full travel of both elevators.

- Move the F/O stick from right stop to left stop, thenfrom forward stop to aft stop.Each stop must be applied during 3 s




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-94 SEC System

(Spoiler and

Elevator

Computer)

27-94-01 SEC 1


- On the F/CTL SD page, check the correct movement

of the pairs of spoilers 2 and 5 and the full travel of both elevators.

CAUTION



attempt any reset.





- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On





30 JUN 12MEL

A320/321MEL/CDL 01.27.49

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


and Elevator

Computer)

27-94-01 SEC 1


IN FLIGHT

Do not use the speedbrakes.

- If the SEC 2 and the SEC 3 fail during the flight:

Autoland is not permitted.

Maximum landing capability is CAT I

Disengage the AP at 500 ft RA before landing in directlaw.

When the AP is disengaged with the three SECsfailed, it cannot be engaged again.


Refer to AMM 27-94-00-040-002



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-94 SEC System

(Spoiler and

Elevator

Computer)

27-94-02 SEC 2

27-94-02A B 1 0 (O)(M) May be inoperative provided that:


2) The SEC 1 and the SEC 3 are operative, and

3) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRSare operative, and

4) All aileron servo-controls and roll spoilers associatedwith the operative SECs are operative, and

5) The sidestick transducers associated with the ELACsand the operative SECs are checked operative beforeeach flight, and

6) The elevators control through the SEC 1 and theELACs and the roll spoilers control through theoperative SECs are checked operative before each

flight.



Note:


available:


System with:










30 JUN 12MEL

A320/321MEL/CDL 01.27.51

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


and Elevator

Computer)

27-94-02 SEC 2


Note:

After application of the maintenanceprocedure, the C/B TRIPPED REAR

PNL N-R alert is displayed on the EWD.

Check of the elevator control through the operative

computers:



- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

- BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . AUTO

- BLUE PUMP OVRD pb. . . . . . . . . . . . . . . . . . . ON

- ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On

- ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On

- SEC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On

- Wait 5 s

Check of the elevator control through the ELAC 1:




- Wait 5 s


- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-94 SEC System

(Spoiler and

Elevator

Computer)

27-94-02 SEC 2


- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- Move the CAPT stick from forward stop to aft stop.

- On the F/CTL SD page, check the full travel of bothelevators.

CAUTION

If an expected elevator movement does



Check of the elevator control through the SEC 1:

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- Wait 5 s



- On the F/CTL SD page, check that the blue elevator actuator symbols becomes amber.

- Wait 5 s


- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- Move the CAPT stick from right stop to left stop, thenfrom forward stop to aft stop.Each stop must be applied during 3 s



30 JUN 12MEL

A320/321MEL/CDL 01.27.53

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


and Elevator

Computer)

27-94-02 SEC 2



Each stop must be applied during 3 s


CAUTION



attempt any reset.





- ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

- ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On

AFTER ENGINE START

Note:

The F/CTL ELEV SERVO FAULT alert

may be displayed on the EWD if the

PTU is inhibited and only one engine is

operating. This alert must disappear when the PTU or the second engine is

started.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-94 SEC System

(Spoiler and

Elevator

Computer)

27-94-02 SEC 2


IN FLIGHT




Disengage the AP at 500 ft RA before landing in direct law.

When the AP is disengaged with the three SECs failed, it

cannot be engaged again.


Refer to AMM 27-94-00-040-002

27-94-03 SEC 3


1) The SEC 1 and SEC 2 are operative, and


3) All aileron servo-controls and roll spoilers associatedwith the operative SECs are operative, and

4) The Flight Manual performance penalties for the pairsof spoilers 1 and 2 inoperative are applied.


30 JUN 12MEL

A320/321MEL/CDL 01.27.55

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS


and Elevator

Computer)

27-94-03 SEC 3





Deactivation of the SEC 3:

- SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

- FLIGHT CONTROLS/SEC 3/SPLY (121VU Q19)C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull

IN FLIGHT




Disengage the AP at 500 ft RA before landing in directlaw.

When the AP is disengaged with the three SECsfailed, it cannot be engaged again.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROLS

27-94 SEC System

(Spoiler and

Elevator

Computer)

27-95-01 FCDC 1


27-95-02 FCDC 2




FLIGHT CONTROLS/FCDC2/SPLY (121VU Q20) C/B· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull

* * *

30 JUN 12MEL

A320/321MEL/CDL 01.27.57

FLIGHT CONTROLS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




A320/321MEL/CDL

MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-00 MAINTENANCE

Message on the

STATUS SD page

28-00-01 FUEL

MAINTENANCE

Message

28-00-01A C 1 - FUEL MAINTENANCE message may be displayed on the

STATUS SD page.


28-01-01 FUEL Overhead

Panel

28-01-01-01 Wing TK PUMP

pb-sw FAULT

light


corresponding pump is set to OFF when the associated

tank is empty.

28-01-01-02 Wing TK PUMP

pb-sw OFF light


corresponding pump indication is operative on the FUEL

SD page.

28-01-01-03 X FEED pb-sw

ON light

28-01-01-03A C 1 0 May be inoperative provided that the X FEED indication is

operative on the FUEL SD page.

28-01-01-04 X FEED pb-sw

OPEN light

28-01-01-04A C 1 0 May be inoperative provided that the X FEED indication is


12 FEB 12MEL

A320/321MEL/CDL 01.28.01

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL



Panel

28-01-01-05 CTR TK PUMP

pb-sw FAULT

light

(A320)

28-01-01-05A C 2 0 One or both may be inoperative provided that the

corresponding pump is set to OFF when there is no fuel in

the center tank.

28-01-01-05 CTR TK XFR pb-

sw FAULT light

(A321)


corresponding transfer valve is set to OFF when there is

no fuel in the center tank.

28-01-01-06 CTR TK PUMPpb-sw OFF light

(A320)


corresponding pump indication is operative on the FUEL

SD page.

28-01-01-06 CTR TK XFR pb-

sw OFF light

(A321)


corresponding transfer valve indication is operative on theFUEL SD page.

01.28.02FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL



Panel

28-01-01-07 FUEL MODE

SEL pb-sw

FAULT light

(A320)

28-01-01-07A C 1 0 (O) May be inoperative provided that all tank pumps

indications are operative on the FUEL SD page.


AFTER ENGINE START

- If there is fuel in the center tank and with the slatsretracted:On the FUEL SD page, check that the center tankpumps indications are in line.

- With the slats extended:

On the FUEL SD page, check that the center tank

pumps indications are cross line.

AFTER TAKEOFF

- If there is fuel in the center tank and with the slatsretracted:On the FUEL SD page, check that the center tankpumps indications are in line.

28-01-01-07 FUEL MODE

SEL pb-sw

FAULT light

(A321)

28-01-01-07B C 1 0 May be inoperative provided that all wing tank pumps and

center tank transfer valves indications are operative on the

FUEL SD page.

12 FEB 12MEL

A320/321MEL/CDL 01.28.03

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL



Panel

28-01-01-08 ACT pb-sw

FAULT light

(A320) (ACTs)

28-01-01-08A C 1 0 (O) May be inoperative provided that the fuel quantity

indications of the ACT(s) and of the center tank are



IN FLIGHT

- If a manual transfer from the ACT to the CTR tankis necessary:

- Refer to FCOM/PRO-ABN-28 ACT XFR FAULT PROC .

- On the FUEL SD page, monitor the fuel transfer.

28-01-01-09 ACT pb-sw FWD

light (A320)

(ACTs)


01.28.04FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page

28-07-01 Fuel Quantity

Indications on

the FUEL SD

page

28-07-01-01 Fuel On Board

(FOB) Indication

on the FUEL SD

page



AFTER ENGINE START

Check that /FF is selected on the MCDU FUEL PREDpage.

- If /FF is not selected on the MCDU FUEL PREDpage:

Insert the FOB.

The FOB may be calculated either using theindications on the refuel control panel (if available)or by using the Manual Magnetic Indicators(MMIs):Refer to FCOM/LOD-FUL-FUEL-C USE OF MANUAL MAGNETIC INDICATIOR (MMI)

12 FEB 12MEL

A320/321MEL/CDL 01.28.05

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-02 Fuel Quantity

Indication (FQI)

in Degraded

Mode on the

FUEL SD page

28-07-01-02A (A320 ACTs)

(A320)

(A321)

C

C

C

6

5

3

0

0

0

(O) One or more FQI may be in the degraded mode (with

dashes on the two last digits) provided that the loss of

accuracy is taken into account for the fuel planning for

each affected tank.

Note:

The Fuel On Board indication is also in

the degraded mode.


ON GROUND

The FQI is in degraded mode when the FOB indication is

displayed with two dashes across the two last digits on the

EWD.

- When the FQI is in degraded mode:

On the FUEL SD page, determine which tank isaffected.The resulting loss of accuracy must be taken into

account by using the two following parameters:

1. Fq : The extra fuel quantity to be loaded.

2. W: The weight to be added to the total fuel weightfor TOW calculation only.

Fq and W parameters are given as follows :


01.28.06FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page


Indication (FQI)

in Degraded

Mode on the

FUEL SD page

28-07-01-02A (Cont’d) OPERATING PROCEDURES(Cont’d)

Applicable to (A320)

LOSS OF ACCURACY DUE TO THE FUEL QUANTITYINDICATION IN DEGRADED MODE

(Values in kg)

Fq(kg) W (kg)

OUTER TANK 20 200

INNER TANK 110 110

CENTER TANK 130 130

ALL TANKS 390 750

- When the auto refuel stops:

- Preselect the fuel quantity required for the mission :Fm

- Enter the table and determine Fq and W values for the affected tank.

- Start again the auto refuel with the new preselectedquantity which corresponds to the total FOB :Fm+Fq


12 FEB 12MEL

A320/321MEL/CDL 01.28.07

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page


Indication (FQI)

in Degraded

Mode on the

FUEL SD page

28-07-01-02A (Cont’d) OPERATING PROCEDURES (A320)

Note:

If all tanks reach high level before

having loaded the complete Fq value,

this shows that all tanks are

volumetrically full but the necessary fuel

mass for the mission is not guaranteed

since the fuel quantity indication varieswith the fuel density. Therefore the

mission or the aircraft load must be

amended to match the minimum fuel

quantity known to be onboard.

- When the auto refuel stops again:

The FOB value to be considered for TOW calculationis: FOB = Fm+Fq+W

- If all tanks reach high level before havingloaded Fq value:- The extra fuel quantity known to be onboard is

Fq* with: Fq* < Fq

- The FOB value to be considered for TOWcalculation is: FOB = Fm+Fq *+W

- If the resulting TOW is higher than the MTOW:

The aircraft load must be reduced.


01.28.08FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page


Indication (FQI)

in Degraded

Mode on the

FUEL SD page

28-07-01-02A (Cont’d) OPERATING PROCEDURES (A321)

ON GROUND

The FQI is in degraded mode when the FOB indication is

displayed with two dashes across the two last digits on the

EWD.

- When the FQI is in degraded mode:

On the FUEL SD page, determine which tank isaffected.The resulting loss of accuracy must be taken intoaccount by using the two following parameters:

1. Fq : The extra fuel quantity to be loaded.

2. W: The weight to be added to the total fuel weightfor TOW calculation only.


12 FEB 12MEL

A320/321MEL/CDL 01.28.09

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page


Indication (FQI)

in Degraded

Mode on the

FUEL SD page

28-07-01-02A (Cont’d) OPERATING PROCEDURES (A321) (Cont’d)

Fq and W parameters are given as follows :

LOSS OF ACCURACY DUE TO THE FUEL QUANTITYINDICATION IN DEGRADED MODE

(Values in kg)

Fq(kg) W (kg)

WING TANK 130 310

CENTER TANK 130 130

ALL TANKS 390 750

- When the auto refuel stops:

- Preselect the fuel quantity required for the mission: Fm

- Enter the table and determine Fq and W values for the affected tank.

- Start again the auto refuel with the newpreselected quantity which corresponds to the

total FOB : Fm+Fq


01.28.10FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page


Indication (FQI)

in Degraded

Mode on the

FUEL SD page

28-07-01-02A (Cont’d) OPERATING PROCEDURES (Cont’d)

Applicable to (A321)

Note:

If all tanks reach high level before

having loaded the complete Fq value,

this shows that all tanks are

volumetrically full but the necessary fuel

mass for the mission is not guaranteedsince the fuel quantity indication varies

with the fuel density. Therefore the

mission or the aircraft load must be

amended to match the minimum fuel

quantity known to be onboard.

- When the auto refuel stops again:

The FOB value to be considered for TOW calculationis: FOB = Fm+Fq+W

- If all tanks reach high level before having loaded Fqvalue:

- The extra fuel quantity known to be onboard isFq* with: Fq* < Fq

- The FOB value to be considered for TOW

calculation is: FOB = Fm+Fq *+W

- If the resulting TOW is higher than the MTOW:

The aircraft load must be reduced.

12 FEB 12MEL

A320/321MEL/CDL 01.28.11

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-03 Outer Tank Fuel

Quantity

Indication on the

FUEL SD page

(A320)

28-07-01-03A Check of fuel

quantity in the

associated tank

after refueling

C 2 1 (O)(M) One may be inoperative provided that:

1) The fuel quantity in the associated tank is checkedafter each refueling by the corresponding fuel quantityindicator on the refuel/defuel control panel, and

2) The associated fuel used indication is operative, and

3) The associated inner tank indication is operative.


AFTER REFUELING

To check the fuel quantity in the associated tank:Refer to FCOM/PER-LOD-FUL-FUEL-A. GENERALINFORMATION.


Refer to AMM 28-40-00-040-003

28-07-01-03B High level fuel

detection

system checkedoperative

before refueling

and associated

inner tank

indication

operative

C 2 1 (M) One may be inoperative provided that:

1) The high level fuel detection system is checked

operative before refueling, and

2) The tanks in both wings are full, and

3) The associated fuel used indication is operative, and

4) The associated inner tank indication is operative.


Refer to AMM 28-40-00-040-003

01.28.12FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-03 Outer Tank Fuel

Quantity

Indication on the

FUEL SD page

(A320)

28-07-01-03C Check of fuel

quantity in the

associated wing

after refueling/

defueling

B 2 1 (O)(M) One may be inoperative provided that:

1) The fuel quantity in the associated wing (inner andouter tanks) is checked after each refueling/defuelingby the corresponding fuel quantity indicator on therefuel/defuel control panel, and

2) The associated fuel used indication is operative.


Refer to MEL item 28-07-01-03A


Refer to AMM 28-40-00-040-003

28-07-01-03D High level fuel

detection

system checked

operative

before refueling

B 2 1 (M) One may be inoperative provided that:

1) The high level fuel detection system is checkedoperative before refueling, and




Refer to AMM 28-40-00-040-003

12 FEB 12MEL

A320/321MEL/CDL 01.28.13

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-04 Inner Tank Fuel

Quantity

Indication on the

FUEL SD page

(A320)


quantity in the

associated tank

after refueling


1) The fuel quantity in the associated tank is checkedafter each refueling by the corresponding fuel quantityindicator on the refuel/defuel control panel, and



AFTER ENGINE START


- If /FF is not selected on the MCDU FUEL PREDpage:

Insert the FOB.

The FOB may be calculated either using theindications on the refuel control panel (if available)or by using the Manual Magnetic Indicators(MMIs): Refer to FCOM/PER-LOD-FUL-FUEL-C.MANUAL MAGNETIC INDICATOR (MMI)


Refer to AMM 28-40-00-040-005

01.28.14FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-04 Inner Tank Fuel

Quantity

Indication on the

FUEL SD page

(A320)

28-07-01-04B High level fuel

detection

system checked

operative

before refueling






Refer to AMM 28-40-00-040-005

12 FEB 12MEL

A320/321MEL/CDL 01.28.15

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-04 Wing Tank Fuel

Quantity

Indication on the

FUEL SD page

(A321)


quantity in the

associated tank

after refueling


1) The fuel quantity in the associated tank is checkedafter each refueling by the manual magnetic indicatorsor by the corresponding fuel quantity indicator on therefuel/defuel control panel, and



AFTER ENGINE START


- IIf /FF is not selected on the MCDU FUEL PREDpage:

Insert the FOB.

The FOB may be calculated either using theindications on the refuel control panel (if available) or by using the Manual Magnetic Indicators (MMIs): Refer to FCOM/PER-LOD-FUL-FUEL-C.

MANUAL MAGNETIC INDICATOR (MMI).MAINTENANCE PROCEDURE

Refer to AMM 28-40-00-040-005

01.28.16FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-05 Center Tank

Fuel Quantity

Indication on the

FUEL SD page

(A320)


quantity after

refueling


1) The fuel quantity in the center tank is checked after each refueling by the manual magnetic indicators or bythe corresponding fuel quantity indicator on therefuel/defuel control panel, and

2) All wing tanks fuel quantity indications are operative,and

3) Both fuel used indications are operative.


AFTER REFUELING

To check the fuel quantity in the associated tank:Refer to FCOM/PER-LOD-FUL-FUEL-C.MANUAL MAGNETIC INDICATOR (MMI).


Refer to AMM 28-40-00-040-006

28-07-01-05B Fuel in the

center tank not

usable

C 1 0 May be inoperative provided that there is no fuel in the

center tank or the fuel in this tank is considered as not

usable and as part of the ZFW and is taken into account

for CG determination.

12 FEB 12MEL

A320/321MEL/CDL 01.28.17

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page


Fuel Quantity

Indication on the

FUEL SD page

(A320) (ACTs)

Note:

This failure will result in the display of the FUEL ACT XFR FAULT alert while

the automatic transfer is still operative.

Refer to Item 28-09-03 FUEL ACT XFR

FAULT Alert


quantity after

refueling

C 1 0 (O)(M)

(FD)


1) The fuel quantity in the center tank is checked after each refueling by the manual magnetic indicators or bythe corresponding fuel quantity indicator on therefuel/defuel control panel, and

2) All wing tanks and ACT(s) fuel quantity indications areoperative, and

3) Both fuel used indications are operative, and

4) The forward transfer from ACT(s) to the center tank ismonitored during the flight.


AFTER REFUELING

To check the fuel quantity in the associated tank: Refer to

FCOM/PER-LOD-FUL-FUEL-A.GENERAL

INFORMATION.


01.28.18FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page


Fuel Quantity

Indication on the

FUEL SD page

(A320) (ACTs)

28-07-01-05A (Cont’d) OPERATING PROCEDURES (Cont’d)

AT TOP OF CLIMB

- Check on the FUEL SD page that the fuel istransferred from one additional center tank (from ACT2 if ACT 2 is installed and not empty) to the center tank.

- Check that the fuel quantity in one additional center tank has decreased (from ACT 2 if ACT 2 is installedand not empty).

- If the automatic transfer has not started:

- After 30 minutes of flight:

- ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD

- If necessary perform a descent to FL 270.

- When ACT (both ACTs if two ACTs installed)empty:

ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO


Refer to AMM 28-40-00-040-006

28-07-01-05B Fuel in the

center tank not

usable

C 1 0 May be inoperative provided there is no fuel in the center

tank or the fuel in this tank is considered as not usable and

as part of the ZFW and is taken into account for CG

determination.

12 FEB 12MEL

A320/321MEL/CDL 01.28.19

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-06 ACT Fuel

Quantity

Indication on the

FUEL SD page

(A320) (ACTs)

Note:

This failure will result in the inhibition of the FUEL ACT XFR FAULT alert.

Refer to Item 28-09-03 FUEL ACT XFR

FAULT Alert

28-07-01-06B Fuel in the ACT C 1 0 (O)(FD) One fuel quantity indication may be inoperative provided

that:

1) All wing tanks and center tank and the other ACT fuelquantity indications are operative, and

2) Both fuel used indications are operative, and

3) The forward transfer from ACT(s) to the center tank ismonitored during the flight.


AT TOP OF CLIMB

Check of the fuel transfer from one additional center tank

(from ACT 2 if ACT 2 is installed and not empty) to the

center tank:

On the FUEL SD page, check that the transfer indication

(arrow) is displayed or check that the total fuel indicated is

above the actual fuel indicated after refuel minus FU.


- After 30 minutes of flight:- ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD



01.28.20FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page


Indications on

the FUEL SD

page

28-07-01-06 ACT Fuel

Quantity

Indication on the

FUEL SD page

(A320) (ACTs)

28-07-01-06B (Cont’d) OPERATING PROCEDURES (Cont’d)

- When ACT (both ACTs if two ACTs installed) isempty:

ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

28-70-01-06C ACT empty C 1 0 One may be inoperative provided that there is no fuel in

any ACT.

12 FEB 12MEL

A320/321MEL/CDL 01.28.21

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page

28-07-02 Fuel

Temperature

Indications on

the FUEL SD

page

28-07-02-01 Fuel

Temperature

Indication on the

FUEL SD page

(A320)

28-07-02-01A C 4 2 One in each wing or both in one wing may be inoperative.

28-07-02-01 Fuel

Temperature

Indication on the

FUEL SD page

(A321)


01.28.22FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page

28-07-03 Tank Pump

Indications on

the FUEL SD

page

28-07-03-01 Wing Tank

Pump Indication

on the FUEL SD

page



Pump Indication

on the FUEL SD

page (A320)


28-07-04 ValveIndications on

the FUEL SD

page

28-07-04-01 Engine LP Fuel

Valve Indication

on the FUEL SD

page

28-07-04-01A C 2 0 (M) One or both may be inoperative provided that the

associated LP valve is checked operative before each

flight.


Refer to AMM 28-24-00-040-001

12 FEB 12MEL

A320/321MEL/CDL 01.28.23

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page

28-07-04 Valve

Indications on

the FUEL SD

page

28-07-04-02 APU LP Fuel

Valve Indication

on the FUEL SD

page

28-07-04-02A C 1 0 (M) May be inoperative provided that:

1) The APU LP valve is secured in the closed positionand,

2) The APU is not used.


Refer to AMM 28-40-00-040-001

28-07-04-03 Crossfeed Valve

Indication on the

FUEL SD page

28-07-04-03A C 1 0 (M) May be inoperative provided that operation of the

crossfeed valve is checked before the first flight of each

day.


Refer to AMM 28-40-00-040-002

01.28.24FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page

28-07-04 Valve

Indications on

the FUEL SD

page

28-07-04-04 Wing Transfer

Valve Indication

on the FUEL SD

page

(A320)

28-07-04-04A C 2 0 (O)(M) One or both may be inoperative provided that:

1) The fuel quantity indications of the associated inner and outer tanks are operative, and

2) The transfer valve operation is checked before eachflight and when used in flight.


IN FLIGHT

- When any inner tank fuel quantity reaches 750 kgof fuel:

On the FUEL SD page, check the associated outer tank transfer.


Refer to AMM 28-40-00-040-004

12 FEB 12MEL

A320/321MEL/CDL 01.28.25

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


FUEL SD page

28-07-04 Valve

Indications on

the FUEL SD

page


Transfer Valve

Indication on the

FUEL SD page

(A321)


28-07-04-06 ACT to CTR TK

Transfer (Arrow)

Indication on the

FUEL SD page

(A320) (ACTs)

28-07-04-06A C 1 0 May be inoperative provided that the fuel quantity

indications (both FQI if both ACTs installed) of the ACT(s)

and of the center tank are operative on the FUEL SD

page.

01.28.26FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-09 ECAM Alerts

28-09-01 FUEL L(R)

INNER(OUTER)

TK HI TEMP

Alert

(A320)

28-09-01A One or two

inoperative

C 4 2 (O) One in each wing or both in one wing may be displayed

provided that:

1) The fuel temperature indications of the non affectedtanks are operative on the FUEL SD page, and

2) The fuel temperature is monitored before takeoff andduring the flight.

Note:

For fuel temperature limitations, Refer to

FCOM LIMITATION.



On the FUEL SD page, monitor the fuel temperature

before takeoff and periodically during the flight.

Note:

For fuel temperature limits, Refer to

FCOM LIMITATION.

- If fuel temperature reaches limits:

- Before takeoff:

Delay takeoff and shut down the engine on theaffected side.

- In flight:- Increase the engine fuel flow on the affected

side.

- If necessary use the APU GEN and switch off

the IDG on the affected side (if the opposite

GEN is available).

12 FEB 12MEL

A320/321MEL/CDL 01.28.27

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-09 ECAM Alerts

28-09-01 FUEL L(R)

INNER(OUTER)

TK HI TEMP

Alert (A320)

28-09-01B One or more

inoperative

C 4 0 (O) One or more may be displayed provided that:

1) The fuel temperature indications are operative on theFUEL SD page, and


Note:


FCOM LIMITATION.


Refer to MEL item 28-09-01A (A320)

28-09-01 FUEL L(R) WINGTK HI TEMP

Alert (A321)

28-09-01A One inoperative C 2 1 (O) One may be displayed provided that:

1) The fuel temperature indications of the opposite wingare operative on the FUEL SD page, and


Note:


FCOM LIMITATION.


01.28.28FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-09 ECAM Alerts

28-09-01 FUEL L(R) WING

TK HI TEMP

Alert (A321)



On the FUEL SD page, monitor the fuel temperaturebefore takeoff and periodically during the flight.

Note:


FCOM LIMITATION.


- Before takeoff:

Delay takeoff and shut down the engine on theaffected side.

- In flight:

- Increase the engine fuel flow on the affectedside.

- If necessary use the APU GEN and switch off

the IDG on the affected side (if the opposite

GEN is available).

28-09-01B Two inoperative C 2 0 (O) One or both may be displayed provided that:



Note:


FCOM LIMITATION.



12 FEB 12MEL

A320/321MEL/CDL 01.28.29

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-09 ECAM Alerts

28-09-02 FUEL L(R)

INNER(OUTER)

TK LO TEMP

Alert

(A320)

28-09-02A One or two

inoperative

C 4 2 (O) One in each wing or both in one wing may be displayed

provided that:

1) The fuel temperature indications of the non affectedtanks are operative on the FUEL SD page, and


Note:


FCOM LIMITATION.





Note:


FCOM LIMITATION.


- Before takeoff:

Delay takeoff.

- In flight:

Consider descending to a lower altitude and/or increasing the mach to increase the TAT.

01.28.30FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-09 ECAM Alerts

28-09-02 FUEL L(R)

INNER(OUTER)

TK LO TEMP

Alert

(A320)


inoperative

C 4 0 (O) One or more may be displayed provided that:



Note:


FCOM LIMITATION.



28-09-02 FUEL L(R) WINGTK LO TEMP

Alert

(A321)

28-09-02A One inoperative C 2 1 (O) One may be displayed provided that:

1) The fuel temperature indications of the opposite wingare operative on the FUEL SD page, and


Note:


FCOM LIMITATION.


12 FEB 12MEL

A320/321MEL/CDL 01.28.31

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-09 ECAM Alerts

28-09-02 FUEL L(R) WING

TK LO TEMP

Alert

(A321)





Note:


FCOM LIMITATION.


- Before takeoff:

Delay takeoff.

- In flight:

Consider descending to a lower altitude and/or increasing the mach to increase the TAT.

28-09-02B Both

inoperative

C 2 0 (O) One or both may be displayed provided that:



Note:

For fuel temperature limitations, Refer toFCOM LIMITATION.



01.28.32FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-09 ECAM Alerts

28-09-03 FUEL ACT XFR

FAULT Alert

(A320) (ACTs)

28-09-03A ACT empty C 1 0 May be displayed provided that there is no fuel in any

ACT.

28-09-03B ACT fuel

transfer

monitored

C 1 0 (O) May be displayed provided that the forward transfer from

the ACT(s) to the center tank is monitored during the flight.


Refer to Operating Procedures 28-07-01-05A Center Tank

Fuel Quantity Indication on the FUEL SD page

28-12 Tank Venting

System

28-12-01 Overpressure

Protector

between theInner and the

Outer Tank

(A320)

28-12-01A Inner tank

temperature

monitored

C 2 0 (O) One or both may be broken or missing provided that the

fuel temperature of the inner tank is monitored.


GENERAL INFORMATION

The dispatch condition results in an unusual distribution of the fuel quantity: the outer tank of the affected wing will be

partially empty with the transfer valves normally closed.


Fuel management should be performed with care.


12 FEB 12MEL

A320/321MEL/CDL 01.28.33

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-12 Tank Venting System


Protector

between Inner

and Outer Tank

(A320)


ON GROUND AND IN FLIGHT

- After a long taxi or if the outside air temperature ishigh, with the outer tank of the affected wingempty:The FUEL L(R) OUTER TK HI TEMP alert may bedisplayed on the EWD.

- If the FUEL L(R) OUTER TK HI TEMP alert isdisplayed on the EWD:- Disregard the FUEL L(R) OUTER TK HI TEMP

alert.

- Monitor the inner tank fuel temperature during

taxi and in flight to ensure that it decreases and

remains within the temperature limitations.

Note:


FCOM LIMITATION.

- If the inner tank fuel temperature exceeds the

temperature limitations, apply the FUEL L(R)

INNER TK HI TEMP procedure:

Refer to Operating Procedres 28-09-01A(B)

FUEL L(R) INNER(OUTER)/WING TK HI

TEMP Alert.

28-12-01B Transfer valvessecured open C 2 0 (O)(M) One or both may be broken or missing provided that theassociated transfer valves are secured in the open position

after each refueling.


01.28.34FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-12 Tank Venting

System


Protector

between Inner

and Outer Tank

(A320)

28-12-01B (Cont’d) OPERATING PROCEDURES

GENERAL INFORMATION

The dispatch condition results in an unusual distribution of

the fuel quantity: the fuel in the outer tank on the affected

side will transfer to the inner tank even when the inner tank

is not empty.

ON GROUND

Do not re-select the refuel power or open the refuel door.

Note:

The transfer valve latch circuit will sendorder to de-latch them and the valves

will close again (they will then operate

normally and open at low level).


Refer to AMM 28-12-00-040-003

12 FEB 12MEL

A320/321MEL/CDL 01.28.35

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-12 Tank Venting System


Protector in the

Vent Surge Tank

28-12-02A C 2 1 (O) One may be broken or missing.


ON GROUND AND IN FLIGHT

- Avoid lateral accelerations in order to reduce thepossibility of fuel spill during taxi and climb out.

- In cruise check that no fuel spillage occurred.

- Check that the FOB is sufficient to reach thedestination with the adequate reserve.


Protector in the

Inner Tank

(A320)



Protector in the

Wing Tank

(A321)


01.28.36FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-12 Tank Venting

System


Protector

between the

Center and the

Inner Tank

(A320)



Protector

between the

Center and the

Wing Tank

(A321)



Protector in the

ACT (A320)

(ACTs)

28-12-05A C 1 0 May be broken or missing provided that the ACT auto

transfer system is considered inoperative.

Refer to Item 28-28-01 ACT Auto Transfer System

12 FEB 12MEL

A320/321MEL/CDL 01.28.37

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-15 Intercell Transfer

System

28-15-01 LH Wing

Transfer Valve

(A320)

28-15-01A One or both

inoperative

open

C 2 0 (O) One or both may be inoperative in the open position.


GENERAL INFORMATION




is not empty.

25-15-01C One inoperative

closed

C 2 1 (O)(M) One may be inoperative in the closed position provided

that the remaining LH wing transfer valve is secured in the

open position after each refueling.


Refer to MEL item 28-15-01A.


Refer to AMM 28-15-00-040-001

01.28.38FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-15 Intercell Transfer

System

28-15-02 RH Wing

Transfer Valve

(A320)


inoperative

open

C 2 0 (O)(FD) One or both may be inoperative in the open position.


GENERAL INFORMATION




is not empty.

28-15-02C One inoperative

closed

C 2 1 (O)(M) One may be inoperative in the closed position provided

that the remaining RH wing transfer valve is secured in the

open position after each refueling.




Refer to AMM 28-15-00-040-002

12 FEB 12MEL

A320/321MEL/CDL 01.28.39

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-20 Distribution

28-20-01 Automatic Fuel

Feed System

(A320)



ON GROUND

- If the center tank is empty for the flight :

- MODE SEL pb-sw . . . . . . . . . . . . . . . . . . . . . MAN

- CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF

- If the center tank is not empty for the flight:

- Before engine start:

MODE SEL pb-sw . . . . . . . . . . . . . . . . . . . . . MAN

- 3 min after engine start :

CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF

- After slats retraction and when the fuel in onewing is less than 5 000 kg:CTR TK PUMP 1 and 2 pb-sw. . . . . . . . . . . . . . On

- When the FUEL CTR TK PUMPS LO PR alert isdisplayed on the EWD:CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF

28-21 Main Fuel Pump

System

28-21-01 Wing Tank

Pump

28-21-01A JP4/JET B notused

C 4 3 One pump may be inoperative provided that JP4/JET B isnot used.

01.28.40FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


System

28-21-01 Wing Tank

Pump

28-21-01B Use of JP4/

JET B

C 4 3 (M) Pump 2 LH or pump 2 RH may be inoperative when

JP4/JET B is used provided that:

1) The fuel return valve is checked operative before each

flight, and2) The fuel temperature is less than 30 °C.


Refer to AMM 28-21-00-040-001

28-21-02 Center Tank

Pump

(A320) (ACTs)

28-21-02A One inoperative C 2 1 (O)(FD) One may be inoperative provided that the flight routespermit a landing at a suitable airport if the remaining center

tank pump fails with fuel in the center tank and in any

ACT(s).



In the case of dispatch with fuel in the center tank, the

remaining center tank pump failure must be considered for

the flight planning. Operator has to ensure that, from any

point of the first part of the route where the center tank is

not empty the aircraft may reach a suitable airportconsidering the fuel quantity (FQ) contained in the center

tank as definitely not usable for the flight planning (as a

consequence of the failure of the remaining center tank

pump).


12 FEB 12MEL

A320/321MEL/CDL 01.28.41

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


System


Pump

(A320) (ACTs)



- X FEED pb-sw · · · · · · · · · · · · · · · · · · · · · · CHECK Off

- Affected CTR TK PUMP pb-sw · · · · · · · · · · · · · · · OFF

< If the fuel quantity in the center tank is less than

200 kg:

- Operative CTR TK PUMP pb-sw · · · · · · · · · · · · · · OFF

< If the fuel quantity in the center tank is more than

200 kg:

- Operative CTR TK PUMP pb-sw · · · · · · · · · · · · · · · On

IN FLIGHT

< If the fuel quantity in the center tank is less than

200 kg:

- Operative CTR TK PUMP pb-sw· · · · · · · Maintain OFF

< If the fuel quantity in the center tank is more than

200 kg:

The fuel in the center tank can be completely used if the

operative center tank pump does not fail before the center

tank is empty. If the operative center tank pump fails

before the center tank is empty, consider the fuel quantityremaining and the time to destination to decide either to

continue the flight or to divert.


01.28.42FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


System


Pump

(A320) (ACTs)


· When the fuel quantity in the first wing inner tank is

less than 4 500 kg:

Operative CTR TK PUMP pb-sw . . . . . . . . . . . . . . . . . OFF

X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

· When the fuel quantity in the first wing inner tank

increases above 5 500 kg:

X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off

Operative CTR TK PUMP pb-sw . . . . . . . . . . . . . . . . . OFF

· When the fuel quantity in the center tank is less

than 250 kg:

X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off

12 FEB 12MEL

A320/321MEL/CDL 01.28.43

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


System


Pump

(A320)

28-21-02A One inoperative C 2 1 (O)(FD) One may be inoperative in the closed position provided

that the flight routes permit a landing at a suitable airport if

the remaining center tank transfer valve fails with fuel in

the center tank.


IN FLIGHT

- Disregard the FUEL L(R) XFR VALVE FAULT alertdisplayed on the EWD.

- MODE SEL pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · Auto

- Operative CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · On

- Affected CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · OFF

- When differences between fuel quantities in twowings is above 1 500 kg:Monitor the fuel imbalance.

Note:

Apply the FUEL IMBALANCE FCOM

procedure as required provided that no

fuel leak is suspected.

- Until the fuel is balanced:

L(R) TK PUMPS (on the lighter side) pb-sw . . OFF

28-21-03 Wing Tank

Pump Sequence

Valve

(A320)


pump is set to OFF when the center tank is feeding.

01.28.44FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-22 APU Fuel Pump

System

28-22-01 APU Fuel Pump



FOR APU START OPERATION

Pressurize the LH fuel manifold with at least one fuel tank

pump.

28-22-01B A 1 0 (O)(FD) May be inoperative for four flights.



28-23 Crossfeed System

28-23-01 Crossfeed Valve


12 FEB 12MEL

A320/321MEL/CDL 01.28.45

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-24 Engine LP Fuel

Shutoff

28-24-01 Engine LP Fuel

Valve Electrical

Motor

28-24-01A C 4 3 (M) One may be inoperative on one engine provided that:

1) The affected motor is deactivated, and

2) The remaining motor is checked operative.


Refer to AMM 28-24-00-040-002

28-25 Refuel/Defuel System


Preselector


28-25-02 Fuel Quantity onthe

Refuel/Defuel

Control Panel

28-25-02A (A320 ACTs)

(A320)

(A321)

C

C

C

8

7

5

0

0

0

One or more indications may be inoperative provided that

the fuel quantity is continuously monitored on the FUEL

SD page during refueling and defueling.

28-25-03 Refuel Valve

28-25-03A Manual

refueling

C 3 0 (M) One or more may be inoperative provided that the aircraft

is manually refueled.


Refer to AMM 28-25-00-040-005

01.28.46FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-25 Refuel/Defuel

System

28-25-03 Refuel Valve

28-25-03B Gravity

refueling

C 3 0 One or more may be inoperative provided that overwing

gravity refueling is performed.

Refer to FCOM/PER-LOD-FUL OVERWING GRAVITY

REFUELING

28-25-04 Transfer Defuel

Valve

28-25-04A C 1 0 (M) May be inoperative provided that the valve is secured in

the closed position.


Refer to AMM 28-25-00-040-004

28-25-05 Exterior

Refuel/Defuel

Control Panel

(A320)

28-25-05A Cockpit Fuel

Quantity pre-

selector

operative

C 1 0 (M) May be inoperative provided that the cockpit fuel quantity

pre-selector is operative.


Refer to AMM 28-25-00-040-008

28-25-05 Exterior

Refuel/Defuel

Control Panel

(A321)

28-25-05A C 1 0 (M) May be inoperative provided that the aircraft is manually

refueled.


Refer to AMM 28-25-00-040-008

12 FEB 12MEL

A320/321MEL/CDL 01.28.47

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-26 Main Transfer System


Transfer Valve

(A321)

28-26-01B One Inoperative

Closed

C 2 1 (O) One may be inoperative in the closed position provided

that the flight routes permit a landing at a suitable airport if

the remaining center tank valve fails with fuel in the center

tank.


IN FLIGHT

- Disregard the FUEL L(R) XFR VALVE FAULT alertdisplayed on the EWD.

- MODE SEL pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · Auto

- Operative CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · On

- Affected CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · OFF

· When differences between fuel quantities in two

wings is above 1 500 kg:

Monitor the fuel imbalance.

Note:

Apply the FUEL IMBALANCE FCOM

procedure as required provided that no

fuel leak is suspected.

Refer to FCOM/PRO-ABN-28 FUEL

IMBALANCE.

· Until the fuel is balanced:

L(R) TK PUMPS (on the lighter side) pb-sw . . . . . . . . OFF

01.28.48FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-28 Additional Center

Tank Transfer

System

28-28-01 ACT Auto

Transfer System

(A320) (ACTs)

28-28-01A ACT empty C 1 0 (FD) May be inoperative provided that there is no fuel in any

ACT.

28-28-01B Manual fuel

transfer

operative

C 1 0 (O)(FD) May be inoperative provided that:

1) The manual transfer from the ACT(s) to the center tank is operative, and

2) The fuel quantity indications of the ACT(s) and of thecenter tank are operative on the FUEL SD page.



1. The refuel panel door must be open to check theoperation of the manual transfer on the ground usingthe FUEL SD page. Establish ground communicationsand ensure that the refuel panel door is open duringfollowing check and closed after the check is done.


12 FEB 12MEL

A320/321MEL/CDL 01.28.49

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


Tank Transfer System

(A320) (ACTs)

28-28-01 ACT Auto

Transfer System

28-28-01B (Cont’d) OPERATING PROCEDURES (Cont’d)

2. The manual transfer may be performed only if the

center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor maybe overridden by keeping pressed in the HI LVL pbtest of the refuel panel. When the high level sensor isoverridden, take care to not overfill the center tank.Otherwise, fuel may spill out from the surge tanks.

- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD

- On the FUEL SD page, check that the fuel istransferred from one ACT (from ACT 2 if ACT 2 isinstalled and not empty) to the center tank.

- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

30 MIN AFTER TAKEOFF

- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD

- On the FUEL SD page, check that the fuel istransferred from the ACTs to the center tank.



ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

28-28-01C ACT fuel not

usable

C 1 0 (O)(M)

(FD)


1) The fuel in the ACT(s) is considered as not usable and

as part of the ZFW and is taken into account for CGdetermination, and

2) The ACT transfer valve is secured in the closedposition.


01.28.50FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


Tank Transfer

System (A320)

(ACTs)

28-28-01 ACT Auto

Transfer System

28-28-01C (Cont’d) OPERATING PROCEDURES


When there is less than 3 000 kg of fuel in thecenter tank:Disregard and clear the FUEL ACT XFR FAULT alertdisplayed on the EWD.


Refer to AMM 28-28-00-040-009

28-28-02 ACT Transfer

Valve

28-28-02A Valve closed

with the ACT

empty

C 1 0 (FD) May be inoperative in the closed position provided that

there is no fuel in any ACT.

28-28-02C Valve closed

with the ACT

fuel not usable

C 1 0 (O)(M)

(FD)


1) It is secured in the closed position, and

2) The fuel in the ACT(s) is considered as not usable andas part of the ZFW and is taken into account for CGdetermination.



- When there is less than 3 000 kg of fuel in thecenter tank:Disregard and clear the FUEL ACT XFR FAULT alertdisplayed on the EWD.


Refer to AMM 28-28-00-040-010

12 FEB 12MEL

A320/321MEL/CDL 01.28.51

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL



(A320) (ACTs)

28-28-03 ACT Transfer

Pump


28-28-04 ACT Air Shutoff

Valve

28-28-04A C 1 0 (FD) May be inoperative provided that the ACT auto transfer

system is considered inoperative.


28-28-05 ACT Inward

Pressure Relief

Valve

28-28-05A Valve open with

fuel in the ACT

C 1 0 (O)(FD) May be inoperative in the open position provided that:





1. The refuel panel door must be open to check theoperation of the manual transfer on the ground usingthe FUEL SD page. Establish ground communicationsand ensure that the refuel panel door is open duringfollowing check and closed after the check is done.


01.28.52FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


Tank Transfer

System (A320)

(ACTs)

28-28-05 ACT Inward

Pressure Relief

Valve

28-28-05A Valve open with

fuel in the

ACT(Cont’d)


2. The manual transfer may be performed only if thecenter tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor maybe overridden by keeping pressed in the HI LVL pbtest of the refuel panel. When the high level sensor isoverridden, take care to not overfill the center tank.Otherwise, fuel may spill out from the surge tanks.

- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD

- On the FUEL SD page, check that the fuel istransferred from one ACT (from the ACT 2 if the ACT 2is installed and not empty) to the center tank.

- ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

AT TOP OF CLIMB

Check that the fuel is transferred from the ACTs to the

center tank.


- After 30 min of flight:

- ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD



ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

28-28-05B ACT empty C 1 0 (FD) May be inoperative provided that there is no fuel in any

ACT.

12 FEB 12MEL

A320/321MEL/CDL 01.28.53

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL



(A320) (ACTs)

28-28-06 ACT Vent Valve

28-28-06A Use of ACT fuel C 1 0 (O)(M) May be inoperative in the open position provided that:




Refer to Operating Procedures 28-28-01B ACT Auto

Transfer System (Manual transfer from the ACT(s) to the

center tank operative)


Refer to AMM 28-28-00-040-003

28-28-06B ACT fuel notusable C 1 0 (O)(M)(FD) May be inoperative provided that:1) The fuel in the ACT(s) is considered as not usable and

as part of the ZFW and is taken into account for CGdetermination, and






Refer to AMM 28-28-00-040-011

01.28.54FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


Tank Transfer

System (A320)

(ACTs)

28-28-06 ACT Vent Valve

28-28-06E ACT empty C 1 0 (FD) May be inoperative provided that there is no fuel in any

ACT.

28-28-07 ACT Refuel

Valve


Note:

If the refuel valve is inoperative in the

closed position, the ACT cannot be

refuelled.

28-28-08 ACT IntegratedImpact Wall

28-28-08A Heat shield not

damaged

C 1 1 (M) The protection cover of the ACT integrated impact wall

may be damaged provided that the heat shield is not

damaged.


Refer to AMM 28-28-00-040-006

12 FEB 12MEL

A320/321MEL/CDL 01.28.55

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL



(A320) (ACTs)

28-28-09 ACT 1 Inlet

Valve

28-28-09B All ACTs empty C 1 0 (FD) May be inoperative in the closed position provided that

there is no fuel in the ACT.

28-28-09C ACTs fuel not

usable

C 1 0 (O)(M)

(FD)

May be inoperative in the closed position provided that:

1) The fuel in the ACT is considered as not usable and aspart of the ZFW and is taken into account for CGdetermination, and






Refer to AMM 28-28-00-040-008

01.28.56FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


Tank Transfer

System (A320)

(ACTs)

28-28-09 ACT 1 Inlet

Valve

28-28-09D Use of ACT fuel C 1 0 (M) May be inoperative in the open position provided that the

ACT transfer valve is checked operative before each flight

when the ACT is used.


Refer to AMM 28-28-00-040-004

28-29 APU LP Fuel Shutoff

28-29-01 APU LP Fuel

Valve

28-29-01A Checked closedon FUEL SD

page


1) It is checked closed on the FUEL SD page, and



BEFORE ENGINE START

The APU is not available.

APU MASTER SW pb-sw . . . . . . . . . . . . . . . . . . . . . . . . Off


12 FEB 12MEL

A320/321MEL/CDL 01.28.57

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL



28-29 APU LP Fuel Shutoff

28-29-01 APU LP Fuel

Valve


Note:

i. No APU bleed air will be available for the

Main Engine Start (MES) or the air

conditioning.

ii. No electrical power will be available from the

APU generator.

On the FUEL SD page, check that the APU LP valve is

indicated closed:

Refer to FCOM/DSC-28-20 ECAM FUEL PAGE.

28-29-01B Secured closed C 1 0 (M) May be inoperative provided that:

1) It is secured in the closed position, and



Refer to AMM 28-29-00-040-002

01.28.58FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-43 Manual Magnetic

Indicators

28-43-01 Manual Magnetic

Indicators

(A320)

28-43-01A Associated fuel

quantity

indication

operative on the

FUEL SD page

C 9 0 One or more may be inoperative provided that the

associated fuel quantity indication is operative on the

FUEL SD page.

28-43-01B High level fuel

detection and

fuel used

indication

operative

C 9 0 (M) One or more may be inoperative provided that:





Refer to AMM 28-40-00-040-012

28-43-01 Manual Magnetic

Indicators

(A321)

28-43-01A Associated fuel

quantity

indication

operative on the

FUEL SD page


associated fuel quantity indication is operative on the

FUEL SD page.

28-43-01B High level fuel

detection andfuel used

indication

operative






Refer to AMM 28-40-00-040-012

12 FEB 12MEL

A320/321MEL/CDL 01.28.59

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-46 Tank Level Sensing

28-46-01 High Level

Detection

System in the

Inner Tank

(A320)

28-46-01A C 2 0 One or both may be inoperative provided that the fuel

quantity is continuously monitored during refueling.

28-46-01 High Level

Detection

System in the

Wing Tank

(A321)

28-46-01A C 2 0 One or both may be inoperative provided that the fuel

quantity is continuously monitored during refueling.

28-46-02 High Level

Detection

System in the

Center Tank

28-46-02A C 1 0 May be inoperative provided that the fuel quantity is

continuously monitored during refueling.

01.28.60FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


28-46-02 High Level

Detection

System in the

Center Tank

(A320) (ACTs)

28-46-02A C 1 0 May be inoperative provided that:

1) The fuel quantity is continuously monitored duringrefueling, and

2) The ACT auto transfer system is consideredinoperative.


28-46-03 High Level

Detection

System in the

ACT (A320)

(ACTs)

28-64-03A C 1 0 May be inoperative provided that the fuel quantity iscontinuously monitored during refueling.

28-46-04 Low Level

Detection

System in the

Inner Tank

(A320)


12 FEB 12MEL

A320/321MEL/CDL 01.28.61

FUEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


28 FUEL


28-46-04 Low Level

Detection

System in the

Wing Tank

(A321)


28-46-05 Low Level

Detection

System in the

ACT

(A320) (ACTs)

28-46-05A C 1 0 May be inoperative provided that the ACT auto transfer



28-50 Fuel Management


Indicating

Computer (FQIC)

Channel

28-51-01A A 2 1 (O) One may be inoperative for 10 calendar days.



1. Ensure that correct weights are entered in the FMGCassociated with the affected FQIC channel.

2. In the case of failure in-flight of the remaining FQICchannel, all fuel quantities indications on the EWD arelost.

* * *

01.28.62FUEL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER


29-01-01 HYD Overhead

Panel

29-01-01-01 B(Y) ELEC PUMP

pb-sw FAULT light


associated reservoir quantity indication is operative on the

HYD SD page.

Note:

Simultaneous illumination of the BLUE

ELEC PUMP pb-sw FAULT light and the

ENG 1(2) PUMP pb-sw FAULT light with

engines off may be due to a failed

engine oil low pressure switch. In this

case, the ENG 1(2) OIL LO PR alert is

inoperative.

Refer to Item 79-09-01 ENG 1(2) OIL

LO PR Alert

29-01-01-02 B ELEC PUMP pb-

sw OFF light


29-01-01-03 Y ELEC PUMP pb-

sw ON light


12 FEB 12MEL

A320/321MEL/CDL 01.29.01

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER


29-01-01 HYD Overhead

Panel

29-01-01-04 G(Y) ENG 1(2)

PUMP pb-sw

FAULT light


associated reservoir quantity indication is operative on the

HYD SD page.

Note:



ENG 1(2) PUMP pb-sw FAULT light with




inoperative.


LO PR Alert

29-01-01-05 G(Y) ENG 1(2)

PUMP pb-sw

OFF light


29-01-01-06 PTU pb-sw

FAULT light

29-01-01-06A C 1 0 May be inoperative provided that the quantity indications of

the yellow and green reservoir are operative on the HYDSD page.

29-01-01-07 PTU pb-sw OFF

light


01.29.02HYDRAULIC POWER


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER


29-01-02 Maintenance HYD

Overhead Panel

29-01-02-01 G(B)(Y) LEAK

MEASUREMENT

VALVES pb-sw

OFF light



HYD SD page

29-07-01 Yellow ELEC

Pump Indication

on the HYD SD

page


29-07-02 Pump Indicationon the HYD SD

page


29-07-03 Fire Valve

Indication on the

HYD SD page


12 FEB 12MEL

A320/321MEL/CDL 01.29.03

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER


HYD SD page

29-07-04 PTU Indication

on the HYD SD

page


29-07-05 Reservoir

Quantity

Indication on the

HYD SD page

29-07-05A C 3 2 (M) One may be inoperative provided that:

1) The associated HYD B(G)(Y) RSVR LO LVL alert ischecked operative, and

2) The associated reservoir quantity is checked beforeeach flight.


Refer to AMM task

29-07-06 RAT Indication

on the HYD SD

page

29-07-06A C 1 0 May be inoperative provided that the RAT is visually

checked to be stowed before each flight.

29-07-07 System Label

Indication on the

HYD SD page

29-07-07A C 3 0 (O) One or more may be inoperative provided that theassociated system pressure is checked available before

each flight.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER


HYD SD page

29-07-07 System Label

Indication on the

HYD SD page



Note:


available:


System with:












- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

- Move the CAPT stick left or right.

- On the F/CTL SD page, check the pairs of spoilersmovement.

- YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off - BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · OFF

12 FEB 12MEL

A320/321MEL/CDL 01.29.05

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER


HYD SD page

29-07-08 System

Pressure

Indication on the

HYD SD page

29-07-08A C 3 2 (O) One may be inoperative provided that the associated

system label indication is checked operative before each

flight.



Note:


available:


with:


- The Yellow Engine 2 Pump withthe Engine 2 running.





- If the blue system pressure indication isinoperative:Check of the system label:

- On the HYD SD page, check that the BLUE systemlabel is amber.



- On the HYD SD page, check that the BLUE systemlabel is white and that the arrow is green.





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER


HYD SD page

29-07-08 System Pressure

Indication on the

HYD SD page


- If the yellow system pressure indication is

inoperative:Check of the system label:


- On the HYD SD page, check that the YELLOWsystem label is amber.


- On the HYD SD page, check that the YELLOWsystem label is white and that the arrow is green.


- If the green system pressure indication is

inoperative:Check of the system label:

- On the HYD SD page, check that the GREENsystem label is amber.


- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

- On the HYD SD page, check that the GREENsystem label is white and that the arrow is green.


12 FEB 12MEL

A320/321MEL/CDL 01.29.07

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-09 ECAM Alerts

29-09-01 HYD B(Y) ELEC

PUMP LO PR

Alert

29-09-01A C 2 0 One or both may be displayed provided that the

associated system pressure indication is operative.

29-09-02 HYD B(Y) ELEC

PUMP OVHT

Alert

29-09-02A C 2 0 One or both may be displayed.

29-09-03 HYD G(Y) ENG

1(2) PUMP LO

PR Alert

29-09-03A C 2 0 (O) One or both may be displayed provided that:

1) The associated system pressure indications areoperative, and

2) The engine pumps are checked operative before eachflight.


AFTER ENGINE START

Check of the engines pumps:

- PTU pb-sw· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

- On the HYD SD page, check that the green and theyellow hydraulic systems pressures are correct.

A correct pressure is 3 000 PSI ( ± 200 PSI).

- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-09 ECAM Alerts

29-09-03 HYD G(Y) ENG

1(2) PUMP LO PR

Alert

29-09-03A (Cont’d)) OPERATING PROCEDURES (Cont’d)

Note:

On the HYD SD page, the PTU remainsindicated running .

TAXI

Note:

Due to a false HYD G(Y) ENG 1(2)

PUMP LO PR alert displayed on the

EWD, the “T.O CONFIG NORMAL” line

will not replace the “T.O CONFIG . .

TEST” line in the T.O MEMO.

Consider normal configuration for

takeoff provided that no alert wasdisplayed during the T.O CONFIG TEST

except a false HYD G(Y) ENG 1(2)

PUMP LO PR alert.

CAUTION:

The T.O CONFIG TEST pb must be

maintained pressed to check that there

is no alert except a false HYD G(Y)

ENG 1(2) PUMP LO PR alert.

12 FEB 12MEL

A320/321MEL/CDL 01.29.09

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-09 ECAM Alerts

29-09-04 HYD G(B)(Y)

RSVR LO AIR

PR Alert

29-09-04A C 3 2 (M) One may be inoperative provided that the air pressure is

checked on the associated reservoir before each flight.


Refer to AMM task

29-09-05 HYD G(B)(Y)

RSVR LO LVL

Alert

29-09-05A C 3 2 One may be displayed provided that the associated

reservoir quantity is checked on the HYD SD page before

each flight.

Note:

i. When the alert is displayed on the EWD, theassociated PUMP pb-sw FAULT light and

the PTU pb-sw FAULT light (if the green or

the yellow system is affected) may

simultaneously come on.

Refer to Item 29-01-01-01 B(Y) ELEC

PUMP pb-sw FAULT light, and

Refer to Item 29-01-01-04 G(Y) ENG 1(2)

PUMP pb-sw FAULT light, and

Refer to Item 29-01-01-06 PTU pb-sw

FAULT light

ii. If the blue reservoir is affected, EMER GEN

may appear in the INOP SYS column on theSTATUS SD page before engine start.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-09 ECAM Alerts

29-09-06 HYD G(B)(Y) RSVR

OVHT Alert

29-09-06A C 3 2 The HYD G RSVR OVHT alert or the HYD Y RSVR OVHT

alert may be displayed.

29-09-07 HYD PTU FAULT

Alert

29-09-07A C 1 0 (O) May be displayed provided that the PTU is checked




Note:


available:


System with:- A Ground cart, or with









12 FEB 12MEL

A320/321MEL/CDL 01.29.11

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-09 ECAM Alerts

29-09-07 HYD PTU FAULT

Alert


Check of the PTU:


- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

- On the HYD SD page, check that the green hydraulicsystem pressure indication is green.If the green hydraulic system pressure indication is notavailable, check on the HYD SD page that the GREENsystem label is white and the arrow is green.


29-09-08 HYD RAT FAULT

Alert

29-09-08A C 1 0 (M) May be displayed provided that the RAT integrity is



Refer to AMM task

29-09-09 HYD

G(B)(Y)(B+G)(G+

Y)(B+Y) SYS LO

PR Alert

29-09-09A C 3 0 (O) One or more may be displayed provided that the

associated system pressure is checked available before

each flight.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-09 ECAM Alerts

29-09-09 HYD

G(B)(Y)(B+G)(G+Y)

(B+Y) SYS LO PR

Alert



Note:


available:


System with:












- PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO

- On the CAPT or the F/O side, move the stick left or right.

- On the F/CTL SD page, check the pairs of spoilersmovement.



12 FEB 12MEL

A320/321MEL/CDL 01.29.13

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-10 Main Hydraulic Power

29-10-01 Engine Driven

Pump


29-10-02 Engine Driven

Pump

Depressurizatio

n Function


29-10-03 Blue System

Electric Pump

29-10-03A C 1 1 (O) The automatic control may be inoperative provided that the

pump is manually operated.



- If the blue electric pump continuously runs:

At electrical power supply application:BLUE ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · · · OFF

AFTER ENGINE START

BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . . . . . AUTO

- If the blue electric pump does not automaticallystart:


- On the HYD SD page, check that the blue hydrauliccircuit pressure is available.

AFTER ENGINE SHUTDOWN

BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . . . . . OFF



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-10 Main Hydraulic

Power

29-10-04 Hydraulic System

Accumulator

29-10-04A No hydraulic

fluid leakage

C 3 0 (M) One or more may be inoperative provided that it is

checked that there is no hydraulic fluid leakage in the

accumulator nitrogen charging circuit.


Refer to AMM 29-10-00-040-007

29-10-04B Accumulator

deactivated

C 3 0 (M) One or more may be inoperative provided that the

affected accumulator is deactivated.


Refer to AMM task

29-10-05 Yellow Brake

Accumulator


29-10-07 Engine Pump Fire

Valve


29-10-08 Hydraulic System

Filter

29-10-08A One LP filter

inoperative

C 8 7 One LP filter may be inoperative.

29-10-08B Reservoir filling

filter inoperative

C 8 7 The reservoir filling filter may be inoperative.

12 FEB 12MEL

A320/321MEL/CDL 01.29.15

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-10 Main Hydraulic Power

29-10-09 Hydraulic Case

Drain Filter

29-10-09A C 3 2 (M) One may be inoperative provided that it is removed.


Refer to AMM task

29-22 Blue Auxiliary

Hydraulic Power

29-22-01 Ram Air Turbine


29-23 Power Transfer

29-23-01 Power Transfer

Unit (PTU)

29-23-01A C 1 1 (O) PTU may continuously run when set to AUTO provided

that the operation of the PTU in both directions is checked

before the first flight of each day.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER



Unit (PTU)


AFTER ENGINE START

Check of the PTU operation:

- GREEN ENG 1 PUMP pb-sw . . . . . . . . . . . . . . OFF

- On the HYD SD page, check that the green systempressure is correct.

A correct pressure is 3 000 PSI ( ± 200 PSI).

- Check the PTU arrow indication.

- GREEN ENG 1 PUMP pb-sw . . . . . . . . . . . . . . . On

- PTU pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

- YELLOW ENG 2 PUMP pb-sw . . . . . . . . . . . . . OFF


- Let the pressure in the yellow hydraulic systemdecrease to 200 PSI or less.

- If the pressure is not below 200 PSI, the indicationson the HYD SD page will not be displayed.

- PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO


12 FEB 12MEL

A320/321MEL/CDL 01.29.17

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER



Unit (PTU)


- On the HYD SD page, check that the yellow systempressure is correct.

A correct pressure is 3 000 PSI (± 200 PSI).

- Check the PTU arrow indication.

- YELLOW ENG 2 PUMP pb-sw · · · · · · · · · · · · · · · · On

Note:

i. The PTU pressurizes the system to a

nominal value of 3 000 PSI PSI (± 200 PSI),

but if no consumers are operated the

pressure is not constant. The PTU operates

in a cycle which keeps the pressure in the

hydraulic systems between 2 100 PSI and 3

200 PSI.

ii. For passengers comfort, the PTU may beset to OFF during the taxi after landing

provided that both engines hydraulic pumps

are operative and running. The PTU must be

set back to AUTO before leaving the aircraft.

29-24 Yellow Auxiliary

Hydraulic Power

29-24-01 Yellow System

Electric Pump

29-24-01A C 1 0 (O) May be inoperative provided that the associated pb-sw is

set to off.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


29 HYDRAULIC POWER

29-24 Yellow Auxiliary

Hydraulic Power


Electric Pump


ON GROUND

- If the pump continuously runs and does not stopwhen set to off:DOORS/CARGO (T12 on 122 VU) C/B · · · · · · · · · Pull

- If unsuccessful:

- Y HYD/ELEC PUMP/NORM (AB 03 on 123 VU) C/B. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull

- Y HYD/ELEC/PUMP (AB 06 on 123 VU) C/B. . . Pull

Note:

i. If the pump continuously runs on the

ground, there is a potential overheat

situation.ii. The reset of the C/Bs must be limited

to the time required to open or close

the cargo doors.

* * *

12 FEB 12MEL

A320/321MEL/CDL 01.29.19

HYDRAULIC POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


30 ICE AND RAIN PROTECTION

30-00 MAINTENANCE

Message on the

STATUS SD page

30-00-01 ICE DETECT

MAINTENANCE

Message

30-00-01A One inoperative C 1 - ICE DETECT MAINTENANCE message may be displayed



30-01-01 ANTI ICE

Overhead Panel

30-01-01-01 ANTI ICE ENG

1(2) pb-sw

FAULT light

30-01-01-01A One inoperative C 2 1 (FD) One may be inoperative provided that the associated

engine anti-ice valve is considered inoperative in the

closed position.

Refer to Item 30-21-01A Engine Anti-Ice Valve

30-01-01-01B One or both

inoperative

C 2 0 (FD) One or both may be inoperative provided that the

associated engine anti-ice valve is considered inoperative

in the open position.

Refer to Item 30-21-01 Engine Anti-Ice Valve

30-01-01-02 ANTI ICE ENG

1(2) pb-sw ON

light


12 FEB 12MEL

A320/321MEL/CDL

01.30.01ICE AND RAIN

PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




30-01-01 ANTI ICE

Overhead Panel

30-01-01-03 ANTI ICE WING

pb-sw FAULT

light

30-01-01-03A C 1 0 (O) May be inoperative provided that the anti-ice “arrow”

symbols are operative on the BLEED SD page .



Check of the anti-ice "arrow" symbol:

- Make sure that the engine bleed air supply systemis available.

- ANTI ICE WING pb-sw . . . . . . . . . . . . . . . . . . . . ON

- On the BLEED SD page, check that the anti-ice"arrow" symbols are displayed amber anddisappear after 30 s.

- ANTI ICE WING pb-sw . . . . . . . . . . . . . . . . . . . . Off

30-01-01-03B C 1 0 (M)(FD) May be inoperative provided that the wing anti-ice control

valves are deactivated in the closed position and


Refer to Item 30-11-01 Wing Anti-Ice Control Valve


Refer to AMM 30-11-00-040-002

30-01-01-04 ANTI ICE WING

pb-sw ON light


01.30.02ICE AND RAINPROTECTION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




30-01-02 WIPER

Overhead Panel

30-01-02-01 Wiper High

Speed Function

(FAST Position)


associated low speed function is operative.

30-01-02-02 Wiper Low

Speed Function

(SLOW Position)



BLEED SD page

30-07-01 ANTI ICE

Indication on the

BLEED SD page


30-07-02 Arrow Indication

on the BLEED

SD page


12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-11 Wing Ice Protection

30-11-01 Wing Anti-Ice

Control Valve

30-11-01A Inoperative in

the open

position

C 2 1 (O)(M)

(FD)

The RH valve may be inoperative in the open position

provided that the associated ECAM procedure is applied.



Flight planning:

Increase fuel consumption by:

Zp(ft) 5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000

Fuel penalties 4.5% 4.0% 5.0% 4.0% 4.0% 3.5% 3.0% 2.5%

Single engine cruise:

Decrease drift down ceilings by:

600 ft when OAT £ ISA2 300 ft when OAT > ISA

Approach climb performance:

- When the engine bleed air supply system isclosed:No penalty.

- When the engine bleed air supply system isopen:Decrease maximum climb limiting weight by:1 100 kg when OAT £ ISA + 5° C4 500 kg when OAT > ISA + 5° C


- After application of the maintenance procedure:

On the BLEED SD page, check that the anti-ice arrowsymbol is displayed.The anti-ice arrow symbol may be displayed amber or green.The WING ANTI ICE L(R) HI PR alert must not bedisplayed on the EWD.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-11 Wing Ice

Protection


Control Valve

30-11-01A (Cont’d) OPERATING PROCEDURES (A321) (Cont’d)

BEFORE ENGINE START

- Maintain the X BLEED selector at SHUT before enginestart when the APU bleed is used.

- Start the engine 1.

- Maintain the X BLEED selector at SHUT during thestart of engine 1.

- Use the CROSS BLEED ENGINE START (Refer toFCOM/PRO-SLP-70 Cross Bleed Engine Start)

- Apply the procedure associated with the WING ANTIICE R VALVE OPEN alert displayed on the EWD.

AFTER TAKEOFF

- When above 1 500 ft: Apply the automatic recall of the WING ANTI ICE RVALVE OPEN procedure displayed on the EWD.

IN FLIGHT

- In the case of failure of a Bleed Air Supply System:

PACK (affected side) pb-sw· · · · · · · · · · · · · · · · · · OFF

AFTER LANDING

- Apply the automatic recall of the WING ANTI ICE RVALVE OPEN procedure displayed on the EWD.

12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl





Control Valve



Flight planning:


Zp(ft) 5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000

Fuel penalties 4.5% 4.5% 6.0% 4.5% 3.5% 2.5% 2.5% 2.5%



1100 ft when OAT £ ISA4500 ft when OAT > ISA


- When the engine bleed air supply system isclosed:No penalty.

- When the engine bleed air supply system isopen:Decrease maximum climb limiting weight by:800 kg when OAT £ ISA + 5° C4 900 kg when OAT > ISA + 5° C


- After application of the maintenance procedure:

On the BLEED SD page, check that the anti-ice arrowsymbol is displayed.

The anti-ice arrow symbol may be displayed amber or green.The WING ANTI ICE L(R) HI PR alert must not bedisplayed on the EWD.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-11 Wing Ice

Protection


Control Valve

30-11-01A (cont’d) OPERATING PROCEDURES (A320) (cont’d)

BEFORE ENGINE START

- Maintain the X BLEED selector at SHUT before enginestart when the APU bleed is used.

- Start the engine 1.

- Maintain the X BLEED selector at SHUT during thestart of engine 1.

- Use the CROSS BLEED ENGINE START (Refer toFCOM/PRO-SLP-70 Cross Bleed Engine Start)

- Apply the procedure associated with the WING ANTIICE R VALVE OPEN alert displayed on the EWD.

AFTER TAKEOFF

- When above 1 500 ft: Apply the automatic recall of the WING ANTI ICE RVALVE OPEN procedure displayed on the EWD.

IN FLIGHT

- In the case of failure of a Bleed Air Supply System:

PACK (affected side) pb-sw· · · · · · · · · · · · · · · · · · OFF

AFTER LANDING

- Apply the automatic recall of the WING ANTI ICE RVALVE OPEN procedure displayed on the EWD.


Refer to AMM 30-11-00-040-004

12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl





Control Valve

30-11-01B Inoperative in

the closed

position

C 2 0 (M)(FD)One or both may be inoperative in the closed position

provided tha the aircraft is not operated in known or

forecast icing conditions.


Refer to AMM 30-11-00-040-001

30-21 Engine Air Intake Ice

Protection

30-21-01 Engine Anti-Ice

Valve

30-21-01A Inoperative inthe closed

position

C 2 1 (M)(FD)One may be inoperative in the closed position providedthat the aircraft is not operated in known or forecast icing

conditions.


Refer to AMM 30-21-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-21 Engine Air Intake

Ice Protection


Valve


the open

position

C 2 0 (O)(M)

(FD)

One or both may be inoperative in the open position

provided that the Flight Manual performance penalties are

applied.


GENERAL INFORMATION

An higher idle speed is set on both engines when an

engine anti-ice valve is inoperative in the open position.


Note:

i. For performance calculations

request Modified Tailored Takeoff

and Landing charts (MTTL) from

FPE through Flight Dispatch or usethe following penalties for takeoff

and landing performance

determination if MTTL charts are not

available.

ii. Performance penalties apply

whatever one or both valves are

inoperative.

Takeoff performance:

Perform the takeoff using full thrust (TOGA).


30 JUN 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




Protection


Valve

30-21-01B (Cont’d) OPERATING PROCEDURES (A321) (Cont’d)

Apply the following reductions on the MTOW and the

speeds :

OAT(°C) £ISA+10°C >ISA+10°C

Weight decrement (kg) 900 5100

V1, VR and V2 decrement (kg) 1 5

Flight planning:


Zp (ft) 2 Valves blocked OPEN 1 Valve blocked OPEN

5 000 7.0% 3.5%

10 000 5.0% 2.5%

15 000 5.5% 3.0%

20 000 4.0% 2.0%

25 000 4.0% 2.0%

30 000 3.5% 2.0%

35 000 3.5% 2.0%

40 000 3.5% 2.0%



300 ft when OAT£ ISA + 5°C

2 400 ft when OAT > ISA + 5°C




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




Ice Protection


Valve



Decrease maximum climb limiting weight by:700 kg when OAT £ ISA + 10 °C

5 900 kg when OAT > ISA + 10°C


ANTI ICE ENG (affected) pb-sw. . . . . . . . . . . . . . . ON

AFTER ENGINE START

The FADEC commands the continuous ignition on the

affected engine.


GENERAL INFORMATION

An higher idle speed is set on both engines when an

engine anti-ice valve is inoperative in the open position.


12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




Protection


Valve



Note:

i. For performance calculations request

Modified Tailored Takeoff and Landing

charts (MTTL) from FPE through Flight

Dispatch or use the following penalties for

takeoff and landing performance

determination if MTTL charts are not

available.

ii. Performance penalties apply whatever oneor both valves are inoperative.


Perform the takeoff using full thrust (TOGA).

Apply the following reductions on the MTOW and the

speeds :

OAT(°C) £ISA+10°C ISA+10°C< OAT£ ISA+20°C >ISA+20°C

Weight

decrement

(kg)

1100 2000 3200

V1, VR and

V2

decrement

(kg)

1 1 2




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




Ice Protection


Valve


Flight planning:


Zp (ft) 2 Valves blocked OPEN 1 Valve blocked OPEN

5 000 5.5% 3.0%

10 000 4.5% 2.5%

15 000 4.0% 2.0%

20 000 3.0% 1.5%

25 000 3.0% 1.5%

30 000 2.0% 1.0%

35 000 2.0% 1.0%

40 000 2.0% 1.0%



400 ft when OAT£ ISA + 5°C

3 700 ft when OAT > ISA + 5°C


Decrease maximum climb limiting weight by:

300 kg when OAT £ ISA + 10 °C

4 400 kg when OAT > ISA + 10°C


12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




Protection


Valve



ANTI ICE ENG (affected) pb-sw. . . . . . . . . . . . . . . ON

AFTER ENGINE START

The FADEC commands the continuous ignition on the

affected engine.


Refer to AMM 30-21-00-040-002

30-31 Probe Ice Protection

30-31-01 Probe Heat

Computer (PHC)


probe heating

operative

C 3 2 (M) One may be inoperative provided that the associated

probe heating is checked operative before each flight.


Refer to AMM 30-31-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-31 Probe Ice

Protection

30-31-01 Probe Heat

Computer (PHC)

30-31-01B F/O PHC

inoperative

B 3 2 (O)(M) The F/O PHC may be inoperative provided that the ADRs,

heaters and failure alerts associated with the operative

computers are checked operative every day.



AIR DATA selector· · · · · · · · · · · · · · · · · · · · · · · · F/O 3

IN FLIGHT

- If icing conditions are encountered:

ADR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

CAUTION

When ADR 2 is set to OFF, takeoff in

CONF 1+F is not permitted.

The ADR 2 pb-sw must remain set to OFF for the

remainder of the flight.


Refer to AMM 30-31-00-040-005

12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




30-31-01 Probe Heat

Computer (PHC)

30-31-01C STBY PHC

inoperative

C 3 2 (M)(FD)The STBY PHC may be inoperative provided that:

1) The ADRs, heaters and failure alerts associated withthe operative computers are checked operative everyday, and

2) The aircraft is not operated in visible moisture or inknown or forecast icing conditions, and

3) The OAT at the departure airport is above 5 °C whenthe taxiway or the runway are contaminated with water or slush.


AMM 30-31-00-040-005

30-31-02 Pitot Heater

30-31-02A F/O pitot heater

inoperative

B 3 2 (O)(M)

(FD)

The F/O pitot heater may be inoperative provided that the

ADRs, heaters and failure alerts associated with the CAPTand the STBY probes (pitot, static, AOA, TAT) are

checked operative every day.


Refer to Operations Procedures 30-31-01B Probe Heat

Computer


Refer to AMM 30-31-00-040-002



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-31 Probe Ice

Protection

30-31-02 Pitot Heater

30-31-02B CAPT pitot

heater

inoperative

B 3 2 (M)(FD)The CAPT pitot heater may be inoperative provided that:

1) The ADRs, heaters and failure alerts associated withthe F/O and the STBY probes (pitot, static, AOA, TAT)are checked operative every day, and

2) The aircraft is not operated in visible moisture or inknown or forecast icing conditions.


Refer to AMM 30-31-00-040-002

30-31-02C STBY pitot

heater

inoperative

B 3 2 (M)(FD)The STBY pitot heater may be inoperative provided that:

1) The ADRs, heaters and failure alerts associated with

the CAPT and the F/O probes (pitot, static, AOA, TAT)are checked operative every day, and



Refer to AMM 30-31-00-040-002

12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




30-31-03 Static Ports

Heater

30-31-03A One STBY

static port

heater

inoperative

C 6 5 One STBY static ports heater may be inoperative.

30-31-03B Both STBY

static port

heater

inoperative

C 6 4 (M)(FD)Both STBY static ports heaters may be inoperative

provided that:

1) The ADRs, heaters and failure alerts associated withthe CAPT and the F/O probes (pitot, static, AOA, TAT)are checked operative every day, and

2) The OAT at the departure airport is above 5 °C whenthe runway is contaminated with water or slush.


Refer to AMM 30-31-00-040-003

30-31-03C One or bothF/O static port

heater

inoperative

C 6 5 (O) One F/O static port heaters may be inoperative providedthat the ADRs, heaters and failure alerts associated with

the CAPT and the STBY probes (pitot, static, AOA, TAT)

are checked operative every day.


Refer to Operations Procedures 30-31-01B Probe Heat

Computer

30-31-03D One or both

CAPT static

port heater

inoperative

C 6 5 (M)(FD)One CAPT static port heaters may be inoperative provided

that:


the F/O and the STBY probes (pitot, static, AOA, TAT)are checked operative every day, and

2) The OAT at the departure airport is above 5 °C whenthe runway is contaminated with water or slush.


Refer to AMM 30-31-00-040-003



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-31 Probe Ice

Protection

30-31-04 Angle of Attack

(AOA) Probes

Heating

30-31-04A F/O AOA

inoperative

C 3 2 (O)(M)

(FD)

The F/O AOA probes heating may be inoperative provided

that the ADRs, heaters and failure alerts associated with

the CAPT and the STBY probes (pitot, static, AOA, TAT)

are checked operative every day.



Landing capability CAT II, if icing conditions areencountered during the flight.

RVSM operation are not permitted.


AIR DATA selector· · · · · · · · · · · · · · · · · · · · · · · · F/O 3


Refer to AMM 30-31-00-040-004

30-31-04B STBY AOA

inoperative

C 3 2 (O)(M) The STBY AOA probes heating may be inoperative

provided that the ADRs, heaters and failure alerts

associated with the CAPT and the F/O probes (pitot, static,

AOA, TAT) are checked operative every day





Refer to AMM 30-31-00-040-004

12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl





(AOA) Probes

Heating

30-31-04C CAPT AOA

inoperative

C 3 2 (O)(M)

(FD)

The CAPT AOA probes heating may be inoperative

provided that:


the F/O and the STBY probes (pitot, static, AOA, TAT)are checked operative every day, and





Refer to AMM 30-31-00-040-004

30-31-05 TAT Probes

Heating

30-31-05A One inoperative C 2 1 One may be inoperative.

30-31-05B Both

inoperative

C 2 0 (FD) Both may be inoperative provided that the aircraft is not

operated in visible moisture or in known or forecast icing

conditions.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-42 Windshield Anti-

Icing and

Defogging

30-42-01 Window Heat

Computer

30-42-01A C 2 1 (O)(M)

(FD)


1) The aircraft is not operated in known or forecast icing

conditions, and2) All heaters and failure alerts on the front and sliding

windows associated with the operative computer arechecked operative every day.



Maximum landing capability is CAT I when the PF sideis inoperative.

Landing capability is CAT II when the PNF side isinoperative.


Refer to AMM 30-42-00-040-001

12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-42 Windshield Anti-Icing

and Defogging

30-42-02 Fixed Lateral

Window and

Sliding Window

Heating


30-42-03 Windshield

Heating

30-42-03A C 2 1 (O)(FD) One may be inoperative provided that the aircraft is not

operated in known or forecast icing conditions.



Maximum landing capability is CAT I when the PF sideis inoperative.

Landing capability is CAT II when the PNF side is

inoperative.

30-42-04 PROBES/

WINDOW HEAT

pb-sw AUTO

Control

30-42-04A C 1 0 Automatic control may be inoperative provided that the

PROBES/WINDOW HEAT system is manually selected.

30-42-05 PROBES/

WINDOW HEAT

pb-sw ON light

30-42-05A C 1 0 May be inoperative provided that PROBES/WINDOW

HEATautomatic system is operative.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-45 Windshield Rain

Protection

30-45-01 Windshield

Wiper

30-45-01A One inoperative

on the PNF side

A 2 1 One may be inoperative on the PNF side for three flights.

30-45-01B One inoperative

on the PNF side

C 2 0 (O)(FD) One or both may be inoperative provided that:

1) The aircraft is not operated in precipitation withindeparture and arrival areas, and

2) The approach minima do not require their use.



Maximum landing capability is CAT 1 when the wiper and

the rain repellent are inoperative or deactivated on the PF

side.

30-45-01C Rain repellentsystem

operative

B 2 1 One may be inoperative provided that the associated rainrepellent system is installed and operative.

30-45-02 Windshield

Wiper PARK

Function


inoperative

C 2 0 One or both may be inoperative provided that the

associated wipers can be positioned in a location that will

not obstruct forward vision.

30-45-02B One or both

inoperative andremoved

2 0 (M) One or both may be inoperative provided that the

associated wipers are removed.

Refer to Item 30-45-01 Windshield Wiper


Refer to AMM 30-45-00-040-003

12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-45 Windshield Rain

Protection

30-45-03 Rain Repellent

System


Note:

No entry in the logbook is required whenit is installed but intentionally

deactivated.

30-71 Waste Water Ice

Protection

30-71-01 Waste Water

Drain Mast

Heating System

30-71-01A C 2 0 (M)(FD) One or both may be inoperative provided that:

1) The associated galleys and lavatories are not used,and

2) The associated lavatory water supplies are closed.


Refer to AMM 30-71-00-040-001

30-71-02 Waste Water

Drain Line Ice

Protection

System




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



30-81 Ice Detection

30-81-01 Ice Detection

System



IN FLIGHT

The presence of ice in the vicinity of the windshield and on

the wipers is periodically checked.

30-81-02 External Visual

Icing Indicator

30-81-02A C 1 0 The presence of ice in the vicinity of the winsheild and on

the wipers is periodically checked.

30-81-03 Lighting of

External Visual

Icing Indicator

30-81-03A C 1 0 (O)(FD) May be inoperative.

IN FLIGHT

- If icing conditions are expected during nightoperations:Refer to FCOM limitation for Icing Conditions

* * *

12 FEB 12MEL

A320/321MEL/CDL


PROTECTION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


31 INDICATING/RECORDIG

SYSTEMS

31-00 MAINTENANCE

Message on the

STATUS SD page

31-00-01 QAR

MAINTENANCE

Message

31-00-01A C 1 - QAR MAINTENANCE message may be displayed on the

STATUS SD page.

31-00-02 ACMS

MAINTENANCE

Message

31-00-02A C 1 - ACMS MAINTENANCE message may be displayed on the

STATUS SD page.

31-00-03 DAR

MAINTENANCE

Message

31-00-03A C 1 - DAR MAINTENANCE message may be displayed on the

STATUS SD page.

31-00-04 CFDIU

MAINTENANCE

Message

31-00-04 C 1 - CFDIU MAINTENANCE message may be displayed on the

STATUS SD page.

31-00-05 DMC 1/3

MAINTENANCE

Message

31-00-05A C 2 - DMC 1/3 MAINTENANCE message may be displayed on

the STATUS SD page provided that the DMC 2/3

MAINTENANCE message is not displayed on the STATUS

SD page.

12 FEB 12MEL

A320/321MEL/CDL

01.31.01INDICATING/RECORDING

SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


31 INDICATING/RECORDING

SYSTEMS

31-00 MAINTENANCE

Message on the

STATUS SD page

31-00-06 DMC 2/3

MAINTENANCE

Message

31-00-06A C 2 - DMC 2/3 MAINTENANCE message may be displayed on

the STATUS SD page.


Primary Flight Display

(PFD)

31-05-01 AP Related

Indications on the

FMA

31-05-01A Refer to MEL Item 22-05-01 AP Related Indications on theFMA.

31-05-02 A/THR Related

Indications on the

FMA

31-05-03A Refer to MEL Item 22-05-03 Approach and Landing

Capabilities on the FMA.

31-05-04 Special Messages

on the FMA

31-05-04A Refer to MEL Item 22-05-04 Special Messages on theFMA.

01.31.02INDICATING/RECORDINGSYSTEMS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


Primary Flight

Display (PFD)

31-05-05 Actual Airspeed

Reference Line

and Scale

Indications on the

PFD

31-05-05A Refer to MEL Item 34-05-01 Actual Airspeed Reference

Line and Scale Indication on the PFD

31-05-06 Mach Number

Indication on the

PFD

31-05-06a Refer to MEL Item 34-05-02 Mach Number Indication on

the PFD.

31-05-07 VMO/MMO

CharacteristicSpeed Indication

on the PFD

31-05-07A Refer to MEL Item 34-05-03 VMO/MMO Characteristic

Speed Indication on the PFD.

31-05-08 Altitude Indication

on the PFD

31-05-08A Refer to MEL Item 34-05-04 Altitude Indication on the

PFD.

31-05-09 Vertical SpeedIndication on the

PFD

31-05-09A Refer to MEL Item 34-05-06 Vertical Speed in Inertial

Mode Indication on the PFD

12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS



(PFD)

31-05-10 Other Air Data

Related

Indications on the

PFD

31-05-10A Refer to MEL Item 34-05-07 Other Air Data Related

Indications on the PFD.

31-05-11 Attitude Indication

on the PFD

31-05-11A Refer to MEL Item 34-05-08 Attitude Indication on the

PFD.

31-05-12 Heading Indication

on the PFD

31-05-12A Refer to MEL Item 34-05-09 Heading Indication on thePFD.


Navigation Display

(ND)

31-06-01 Ground Speed

Indication on the

ND

31-06-01A Refer to MEL Item 34-06-01 Ground Speed Indication on

the ND.

31-06-02 True Air Speed

Indication on the

ND

31-06-02A Refer to MEL Item 34-06-02 True Air Speed Indication on

the ND.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


Navigation Display

(ND)


on the ND

31-06-04A Refer to MEL Item 34-06-04 Heading Indication on the ND.

31-06-05 Position (Aircraft

Symbol) Indication

on the ND

31-06-05A Refer to MEL Item 34-06-05 Position (Aircraft Symbol)

Indication on the ND.

31-06-06 Navigation Station

Information on the

ND

31-06-06A Refer to MEL Item 34-06-06 Radio Navaids Indications on

the ND.

31-06-07 Chrono Indication

on the ND

31-06-07A Refer to MEL Item 34-06-07 Chrono Indication on the ND.


System Display

(SD)


System Display

pages

31-07-01A Refer to corresponding item in the associated ATA

chapter.

12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


System Display (SD)

31-07-02 Permanent Data

(TAT, SAT, ISA,

GLOAD - ALT SEL,

UTC, GW)

Indications on the

SD

31-07-02A C 7 1 (O) TAT indication must be available.



Check that the TAT value is operative on the SD

permanent data.

- If the TAT value is not operative:

Check that the TAT value is available through the ADR3.

Note:

Use the AIR DATA SWITCHING

selector to display temporarily the TAT

value on the SD.

IN FLIGHT

- If needed:

The TAT value may be displayed through the sameaction on the AIR DATA SWITCHING selector.


Engine Warning

Display (EWD)

31-08-01 Engine Parameter

Indications on the

EWD

31-08-01A Refer to MEL item 77-08



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


Engine Warning

Display (EWD)

31-08-02 Fuel On Board

(FOB) Indication

on the EWD

31-08-02A Refer to MEL Item 28-07-01-01 Fuel On Board (FOB)

Indication on the FUEL SD page.

31-08-03 MEMO Messages

on the EWD


31-08-04 Slats/Flaps

Position

Indications on the

EWD

31-08-04A Refer to MEL Item 27-08-01 Flap Position Indication on theEWD.

Refer to MEL Item 27-08-02 Slat Position Indication on the

EWD.

Note:

Apply both MEL Items.

31-20 Independent

Instruments

31-20-01 Electrical Clock

Indicator


1) The UTC indication from the CFDIU is operative on thepermanent data of the SD, and

2) A chrono indication is operative on at least one ND.


12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-20 Independent

Instruments

31-20-01 Electrical Clock

Indicator



- After any electrical power interruption resulting inthe loss of the UTC on the SD:Initialize the UTC and the date using the MCDU: Refer to FCOM /DSC-45-20-GMT/Date Initialization.

31-30 Centralized Fault

Display System

(CFDS) and Data

Recording System

31-30-01 Centralized Fault

Display System

(CFDS)


31-30-02 Digital AIDS

Recorder (DAR)

31-30-02A Refer to MEL Item 31-00-03 DAR MAINTENANCE

Message

Note:

Failure of DAR is indicated by a


STATUS SD page.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


Display System

(CFDS) and Data

Recording System

31-30-03 Digital Flight Data

Recorder (DFDR)


1) Cockpit voice Recorder (VCR) is operative,

2) Airplane is not dispatched from JED, RUH, DMM,MED, and

3) Repair are made within 3 flight days.

31-30-04 Data Management

Unit (DMU) part of

Flight Data

Interface and

Management

Unit(FDIMU)

31-30-04 C 1 0 May be inoperative.

31-30-05 Flight Data

Interface Unit

(FDIU)

31-30-05A A 1 0 Note:

If FDIU is inoperative the DFDR and the

QAR are inoperative.

Refer to Item 31-30-03 Digital Flight

Data Recorder (DFDR), and

Refer to Item 31-30-06 Quick AccessRecorder (QAR)

12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


Display System

(CFDS) and Data

Recording System

31-30-06 Quick Access

Recorder (QAR)

31-30-06A Refer to Item 31-00-01 QAR MAINTENANCE Message

Note:

Failure of QAR is indicated by a


STATUS SD page.

31-30-07 Printer


31-38 Up and Down DataLoading System

Acquisition/Interface

and Equipment

31-38-01 DATA LOADING

selector


31-38-02 Data Loading

Routing Box

(DLRB)




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-38 Up and Down Data

Loading System

Acquisition/Interfa

ce and Equipment

31-38-03 Multipurpose Disk

Drive Unit (MDDU)


31-53 Flight Warning

Computer (FWC)

31-53-01 Flight Warning

Computer (FWC)

31-53-01A C 2 1 (O) FWC 2 may be inoperative.




31-53-02 MASTER CAUT

Cancel Function


31-53-03 MASTER WARN

Cancel Function


31-53-04 MASTER CAUT

light


12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-53-05 MASTER WARN

light


31-53-06 Altitude Alert

31-53-06A B 2 1 (O) One altitude alert function May be ioperative.



- When both altitude alert functions are inoperative:


31-53-06B A 2 0 (O)(FD) B oth altitude alert functions may be inoperative provided:

1) Autopilot with altitude hold is operative,

2) Flight is not conducted within RVSM airspace,

3) Enroute operations do not require its use, and

4) Repairs are made within one flight days.

OPERATING PROCEDURES:

1. Flight crew must be aware that the usual alerts for altitude deviations will not occur.

2. PM should call out approaching and departingassigned altitudes.

3. RVSM operations are not allowed.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-55 System Data

Acquisition

Concentrator

(SDAC)

31-55-01 System Data

Acquisition

Concentrator

(SDAC)

31-55-01A C 2 1 SDAC 2 may be inoperative.

31-56 ECAM Control

Panel (ECP)

31-56-01 System Page

Manual Call pb on

the ECP


31-56-02 ALL pb on the

ECP


12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-56 ECAM Control Panel

(ECP)

31-56-03 CLR pb on the

ECP


31-56-04 EMER CANC pb

on the ECP


31-56-05 RCL pb on the

ECP


31-56-06 STS pb on the

ECP

31-56-06A C 1 0 Must be operative.

31-56-07 T.O CONFIG pb on

the ECP



BEFORE TAKEOFF

Check that the aircraft is in the correct takeoff

configuration:

- FLAPS/SLATS· · · · · · · · · · · · · · · · · · · · · · · · · CHECK




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-56 ECAM Control

Panel (ECP)

31-56-07 T.O CONFIG pb on

the ECP


- On EWD, check that the FLAPS position corresponds

to the position inserted in the MCDU PERF TAKE OFFPage.

- PITCH TRIM· · · · · · · · · · · · · · · · · · · · · · · · · · · CHECK

- Check that the selected pitch trim is in the green bandof the pitch trim wheel and corresponds to the valueinserted in the MCDU PERF TAKE OFF Page.

- RUDDER TRIM · · · · · · · · · · · · · · · · · · · CHECK ZERO

- SPEED BRAKE leve · · · · · · · · · · · · · · · · CHECK RET

- SIDESTICK PRIORITY light · · · · · · · CHECK NO RED

- On the WHEEL SD page, check that the brakes

temperature is below 300 °C.

- DOORS · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · CHECK

- On the DOOR/OXY SD page, check that all doors areindicated closed.

- Deselect the DOOR/OXY SD page after the check.

12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-62 Display Management

Computer (DMC)

31-62-01 DMC 1

31-62-01B C 1 0 (O) May be inoperative provided that:

1) The DMC 2 and DMC 3 are operative, and

2) The ISIS airspeed function is operative, and


4) The ISIS attitude function is operative, and


6) The EIS DMC SWITCHING selector is set to CAPT 3.



- In the case of multiple undue ECAM alerts concerningENG 1(2) N1(N2) (EGT)(FF) OVER LIMITOr

ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCYOr NAV ATT(ALT1)(HDG) DISCREPANCYOr NAV FM/GPS POS DISAGREEOr FUEL F.USED/FOB DISAGREEOr MINIMUM or HUNDRED ABOVE callouts, possiblyassociated with EFIS red flags, apply the belowprocedure:

- Crosscheck the affected parameters on the EWD,PFD, ND, or on the related SD page to confirm that

the alerts are undue.- EIS DMC SWITCHING selector . . . . . . . . . . NORM




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-62 Display

Management

Computer (DMC)

31-62-01 DMC 1


Note:

CAPT PFD and ND ae lost when EIS

DMC SWITCHING selector is set to

NORM.

- If the undue ECAM alerts stop:

- Pull EIS/DMC3/SPLY (121 VU Q09) C/B andEIS/DMC3/STBY/SPLY (49 VU E10) C/B for morethan 5 s and push them back.

- EIS DMC SWITCHINGselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . CAPT 3

- If the undue ECAM alerts continue:

- EIS DMC SWITCHING selector. . . . . . . . . . CAPT 3

- Wait for CAPT PFD and ND recovery.

- Pull EIS/DMC2/SPLY (121 VU Q08) C/B for morethan 5 s and push it back.

12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


Computer (DMC)

31-62-02 DMC 2





4) The ISIS attitude function is operative, and


6) The EIS DMC SWITCHING selector is set to F/O 3,and


8) The AC ESS FEED pb-sw FAULT light is checkedoperative every day.



- In the case of multiple undue ECAM alerts concerningENG 1(2) N1(N2) (EGT)(FF) OVER LIMITOr ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCYOr NAV ATT(ALT1)(HDG) DISCREPANCYOr NAV FM/GPS POS DISAGREEOr FUEL F.USED/FOB DISAGREEOr MINIMUM or HUNDRED ABOVE callouts, possiblyassociated with EFIS red flags, apply the belowprocedure:

- Crosscheck the affected parameters on the EWD,PFD, ND, or on the related SD page to confirm thatthe alerts are undue.

- EIS DMC SWITCHING selector . . . . . . . . . . NORM




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-62 Display

Management

Computer (DMC)

31-62-02 DMC 2

31-62-02A OPERATING PROCEDURES (Cont’d)

Note:



NORM.


- Pull EIS/DMC3/SPLY (121 VU Q09) C/B andEIS/DMC3/STBY/SPLY (49 VU E10) C/B for morethan 5 s and push them back.

- EIS DMC SWITCHINGselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F/O 3


- EIS DMC SWITCHING selector . . . . . . . . . . . F/O 3


- Pull EIS/DMC2/SPLY (49 VU E11) C/B for morethan 5 s and push it back.


Refer to AMM 31-68-00-040-005

31-62-03 DMC 3





4) The ISIS attitude indication is operative, and

5) The standby compass is operative.


12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


Computer (DMC)

31-62-03 DMC 3

31-62-03B (cont’d) OPERATING PROCEDURES


- In the case of multiple undue ECAM alerts concerningENG 1(2) N1(N2) (EGT)(FF) OVERLIMITOr ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCYOr NAV ATT(ALT1)(HDG) DISCREPANCYOr NAV FM/GPS POS DISAGREEOr FUEL F.USED/FOB DISAGREEOr MINIMUM or HUNDRED ABOVE callouts, possiblyassociated with EFIS red flags, apply the belowprocedure:

- Crosscheck the affected parameters on the EWD,PFD, ND, or on the related SD page to confirm thatthe alerts are undue.

-EIS DMC SWITCHING selector . . . . . . . . . . . . . . CAPT 3




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-62 Display

Management

Computer (DMC)

31-62-03 DMC 3


Note:



CAPT 3.


- Pull EIS/DMC1/SPLY (49 VU E11) C/B a for morethan 5 s and push it back.

- EIS DMC SWITCHINGselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM


- EIS DMC SWITCHING selector . . . . . . . . . . NORM


- Pull EIS/DMC2/SPLY (121 VU Q08) C/B for morethan 5 s and push it back.

12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS

31-63 Display Unit (DU)

31-63-01 PFDU 1


31-63-02 PFDU 2

31-63-02A C 1 0 (O) May be inoperative provided that PFDU 1, NDU 1, NDU 2,

EWDU and SDU are operative.





PFDU 2 knob · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

31-63-03 NDU 1

31-63-03A C 1 0 (O) May be inoperative provided that PFDU 1, PFDU 2, NDU

2, EWDU and SDU are operative.





NDU 1 knob · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


31-63-04 NDU 2

31-63-04A C 1 0 (O) May be inoperative provided that PFDU 1, PFDU 2, NDU

1, EWDU and SDU are operative.

31-63-05 SDU

31-63-05A A 1 0 (O)(M) May be inoperative for three flight days provided that:

1) The PFDU 1, PFDU 2, NDU 1, NDU 2 and EWDU areoperative, and


3) The AC ESS FEED pb-sw FAULT light is checkedoperative every day.



SDU knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

- In the case of alerts being displayed on the EWD:

Use the ECAM/ND SWITCHING selector to display thesystem page on the selected NDU.

- In the case of failure of the AC BUS 1:

All the Display Units are lost.

Apply the ELEC AC ESS BUS FAULT alert procedure:Refer to FCOM/PRO-ABN-24-ELEC AC ESS FAULT.

Note:

The AC ESS BUS is recovered whenthe AC ESS FEED pb-sw is set to

ALTN.


Refer to AMM 31-68-00-040-006

30 JUN 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


31-63-06 EWDU


31-68 Switching Panel

31-68-01 AIR DATA

SWITCHING

selector on the

Center Pedestal

31-68-01A C 1 0 May be inoperative provided that the AIR DATA

SWITCHING selector is set to NORM.

31-68-02 ATT HDG

SWITCHING

selector on the

Center Pedestal

31-68-02A C 1 0 May be inoperative provided that the ATT HDG


31-68-03 ECAM/ND XFR

SWITCHING

selector on the

Center Pedestal


1) Both ECAM DU are operative, and

2) The ECAM/ND XFR SWITCHING selector is set toNORM.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


31-68-04 EIS DMC

SWITCHING

selector on the

Center Pedestal

31-68-04A C 1 0 May be inoperative provided that the EIS DMC


31-68-05 PFD/ND XFR pb

on the Lateral

Instrument Panel

31-68-05A C 2 0 (O) One or both may be inoperative provided that:

1) The PFD and ND units are operative, and

2) The PFD to ND automatic switching is checkedoperative on the PF side before each flight.



- On the side where the PFD/ND XFR pb isinoperative:

- PFD brightness control knob . . . . . . . . . . . . . . . OFF

- Check that the PFD image is automaticallydisplayed on the NDU.

- PFD brightness control knob . . . . . . . . . . . . . . . . On

- If the PFD image is not automatically displayedon the NDU:The affected side cannot be used by the PilotFlying.


12 FEB 12MEL

A320/321MEL/CDL


SYSTEMS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



SYSTEMS


31-68-05 PFD/ND XFR pb

on the Lateral

Instrument Panel


- On the side where the PFD to ND automaticswitching is inoperative:


- EIS DMC SWITCHING selector (Affected side. . . . . . . . . . . . . . . . . . CAPT 3 (F/O 3)

- Check that the PFD image is displayed on theassociated NDU.

- PFD brightness control knob . . . . . . . . . . . . . . . . On

- EIS DMC SWITCHING knob(Affected side) . . . . . . . . . . . . . . . . . . . . . . . NORM

IN FLIGHT

- If a PFDU fails with no automatic transfer to theassociated NDU:


- EIS DMC SWITCHING selector (Affected side) . . . . . . . . . . . . . . . . . CAPT 3 (F/O 3)

- Check that the PFD image is displayed on theassociated NDU.

* * *



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page

32-07-01A C 4 0 (O) One or more may be inoperative provided that the ground

brake cooling time is applied.



The brake energy graph and the brake cooling time table

given hereafter permit to determine the ground brake

cooling time.

BRAKE ENERGY GRAPH

- If MAX reverser thrust was selected for allreversers during the braking phase:Enter the brake energy graph: WITH THRUST

REVERSERS USE.

- If MAX reverser thrust was NOT selected for allreversers during the braking phase:Enter the brake energy graph: WITHOUT THRUSTREVERSERS USE.

Determination of the brake energy accumulated during a

REJECTED TAKEOFF (RTO) :

- Enter with the aircraft takeoff weight (TOW) and withthe rejected takeoff speed in kt IAS.

- Apply airport pressure altitude, temperature, wind andrunway slope corrections.


LANDING :

- Enter with the aircraft landing weight, and

- Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the manualbraking speed in kt IAS in the other cases.




SEQUENCE


I T E M

12 FEB 12MEL

A320/321MEL/CDL 01.32.01

LANDING GEAR

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page



- Correct for brake setting with a preselected autobrakesetting (LO, MED) or with MAX PEDAL braking in theother cases.

Note:

In the case of a dispatch with one brake

inoperative (Refer to Item 32-42-01

Main Wheel Brake or Refer to Item 32-

42-02 Green System Brake), the brake

energy accumulated is increased by

34%.


01.32.02LANDING GEAR


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page



12 FEB 12MEL

A320/321MEL/CDL 01.32.03

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page



D



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page

32-07-01A (Cont’d) OPERATING PROCEDURES (A320)(Cont’d)

BRAKE COOLING TIME TABLE

Determination of the brake cooling time:

EXAMPLE:

55 152

46

153

46

154

46

155

46

155

47

==> TIME (min) WITHOUT BRAKE

COOLING FAN

==> TIME (min) WITH BRAKE

COOLING FAN

If the Energy and the OAT are not given in the table, use

the values given in the next adjacent column/row.

For Example, with Energy = 78 MJ, and OAT = 15°C,entering the next adjacent column/row (Energy = 80 MJ,

OAT = 20°C) gives the following results:

- Without brake cooling fan: 189 min

- With brake cooling fan: 57 min

Enter the following table with the energy and the OAT to

determine the ground brake cooling time.


12 FEB 12MEL

A320/321MEL/CDL 01.32.05

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page



D



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page



12 FEB 12MEL

A320/321MEL/CDL 01.32.07

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page


AFTER ENGINE START

- In the case of a false BRAKES HOT alert displayedon the EWD:EMER CANC pb · · · · · · · · · · · · · · · · · · · · · · · · · Press

Note:

In the case of a false BRAKES HOT

alert due to a faulty BTMU or a faulty

BSCU, the "T.O CONFIG NORMAL” line

will not replace the "T.O CONFIG . .

TEST" line in the T.O MEMO. Consider

normal configuration for takeoff provided

that no alert were displayed during theT.O CONFIG TEST.

CAUTION


maintained pressed to check that

there is no alert.



The brake energy graph and the brake cooling time table

given hereafter permit to determine the ground brake

cooling time.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page


BRAKE ENERGY GRAPH

- If MAX reverser thrust was selected for allreversers during the braking phase:Enter the brake energy graph: WITH THRUSTREVERSERS USE.

- If MAX reverser thrust was NOT selected for allreversers during the braking phase:Enter the brake energy graph: WITHOUT THRUSTREVERSERS USE.


REJECTED TAKEOFF (RTO) :

- Enter with the aircraft takeoff weight (TOW) and withthe rejected takeoff speed in kt IAS.



LANDING :

- Enter with the aircraft landing weight, and

- Enter with touch down speed in kt IAS if the autobrakewas selected and applied or with the manual brakingspeed in kt IAS in the other cases.


- Correct for brake setting with a preselected autobrakesetting (LO, MED) or with MAX PEDAL braking in theother cases.


12 FEB 12MEL

A320/321MEL/CDL 01.32.09

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page


Note:

In the case of a dispatch with one brake

inoperative (Refer to Item 32-42-01

Main Wheel Brake or Refer to Item 32-

42-02 Green System Brake), the brake

energy accumulated is increased by

34%.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page



12 FEB 12MEL

A320/321MEL/CDL 01.32.11

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page


BRAKE COOLING TIME TABLE

Determination of the brake cooling time:

EXAMPLE:

55 152

46

153

46

154

46

155

46

155

47

==> TIME (min) WITHOUT BRAKE

COOLING FAN

==> TIME (min) WITH BRAKE

COOLING FAN

If the Energy and the OAT are not given in the table, use

the values given in the next adjacent column/row.

For Example, with Energy = 78 MJ, and OAT = 15°C,entering the next adjacent column/row (Energy = 80 MJ,

OAT = 20°C) gives the following results:

- Without brake cooling fan: 189 min

- With brake cooling fan: 57 min

Enter the following table with the energy and the OAT to

determine the ground brake cooling time.


12 FEB 12MEL

A320/321MEL/CDL 01.32.13

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page



12 FEB 12MEL

A320/321MEL/CDL 01.32.15

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-01 Brakes

Temperature

Indication on the

WHEEL SD page


AFTER ENGINE START

- In the case of a false BRAKES HOT alert displayedon the EWD:EMER CANC pb · · · · · · · · · · · · · · · · · · · · · · · · · Press

Note:

In the case of a false BRAKES HOT

alert due to a faulty BTMU or a faulty

BSCU, the "T.O CONFIG NORMAL” line

will not replace the "T.O CONFIG . .

TEST" line in the T.O MEMO. Consider

normal configuration for takeoff provided

that no alert were displayed during theT.O CONFIG TEST.

CAUTION


maintained pressed to check that

there is no alert.

32-07-01B C 4 0 (O)(M) One or more may be inoperative provided that:

1) The associated sensor is deactivated if the BRAKESHOT alert is displayed on the EWD, and

2) The ground brake cooling time is applied.




Refer to AMM 32-47-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-02 L/G Position

Indication on the

WHEEL SD page

32-07-02A C 6 0 One or more may be inoperative provided that the L/G

gear position indications are operative on the LDG GEAR

indicator panel.

32-07-03 L/G Doors

Position Indication

on the WHEEL SD

page



IN FLIGHT

MAX SPEED . . . . . . . . . . . . . . . . . . . . . . . 250 kt or M 0.60

32-07-04 L/G CTL Indication

on the WHEEL SD

page


32-07-05 UP LOCK

Indication on the

WHEEL SD page


32-07-06 [Y] N/W STEERINGIndication on the

WHEEL SD page


12 FEB 12MEL

A320/321MEL/CDL 01.32.17

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-07 Tire Pressure

Indication on the

WHEEL SD page


32-07-08 ANTI SKID, [1], [2]

Indication on the

WHEEL SD page


32-07-09 AUTO BRK

Indication on the

WHEEL SD page


32-07-10 [G] NORM BRK

Indication on theWHEEL SD page


32-07-11 Release Brake

Indication on the

WHEEL SD page




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


WHEEL SD page

32-07-12 ACCU

PRESS/ACCU

ONLY Indication

on the WHEEL SD

page


32-07-13 [Y] ALTN BRK

Indication on the

WHEEL SD page


32-09 ECAM Alerts

32-09-01 BRAKES-N/WS

MINOR FAULT

Alert

32-09-01A Fault on an

alternate

braking system

pressure

transducer

C 1 0 May be inoperative provided that:

1) The alert is confirmed to be caused by a fault on analternate braking system pressure transducer bytroubleshooting, and

2) The associated BRAKES pressure indicator isconsidered inoperative.

Refer to Item 32-44-03 BRAKES Pressure Indicator

12 FEB 12MEL

A320/321MEL/CDL 01.32.19

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-09 ECAM Alerts

32-09-01 BRAKES-N/WS

MINOR FAULT

Alert

32-09-01C Both BRAKES

pressure

indicators

operative

B 1 0 (O)(M) May be displayed provided that:

1) Both BRAKES pressure indicators are operative, and

2) The alternate braking system is checked operativebefore the first flight of each day, and

3) It is checked before each flight that the CFDS failuremessage related to the BRAKES-N/WS MINORFAULT alert do not report a fault on an alternatepressure transducer.



The ACCU PRESS indication must be in the green band.

- If ACCU PRESS indication not in the green band:

Y ELEC PUMP pb-sw · · · · · · · · · · · · · · · ON then OFF

- CHOCKS · · · · · · · · · · · · · · · · · · · · CHECK IN PLACE

- PARKING BRAKE handle · · · · · · · · · · · · · · · · · · · OFF

- PARKING PEDALS · · · · · · · · · · · · · · · · · · · · · PRESS

Apply maximum pressure on both pedals.

- BRAKE PRESSURE(on BRAKES pressure indicators) · · · · · · · · · · CHECK

Pressure must increase without delay symmetricallyon left and right sides for the same applicationsimultaneously applied on left and right pedals. Withfull pedal deflection, the pressure must be between

900 and 1100 psi.

- BRAKES PEDALS · · · · · · · · · · · · · · · · · · · · RELEASE

Check that no residual pressure in the brakes remains.

- PARKING BRAKE handle · · · · · · · · · · · · · · · · · · · · ON


Refer to AMM 32-46-00-040-001



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-09 ECAM Alerts

32-09-02 WHEEL TYRE LO

PR Alert


monitoring

channel

deactivated

C 1 0 (M) May be displayed on one or more wheels provided that:


2) The associated pressure monitoring channel is

deactivated, and

3) The tire pressure on the affected wheel is checked tobe within the limits before the first MEL dispatch andthen every three days.


Refer to AMM 32-49-00-040-001

32-09-02B TPIC

deactivated

C 1 0 (M) May be displayed on all wheels provided that:


2) The Tire Pressure Indicating Computer (TPIC) isdeactivated, and

3) The tire pressure on each wheel is checked to bewithin the limits before the first MEL dispatch and thenevery three days.


Refer to AMM 32-49-00-040-002

01 MAY 12MEL

A320/321MEL/CDL 01.32.21

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-11 Main Gear

32-11-01 Main Gear Torque

Link Damper

32-11-01A A 2 0 (FD) One or both may be inoperative for 7 flights.

32-12 Main Gear Doors

32-12-01 Ground Opening

Cable

32-12-01A C 2 0 (M) One or both may be broken or missing.


Refer to AMM 32-12-00-040-006



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-31 Normal Extension

and Retraction

32-31-01 Landing Gear

Control and

Interface Unit

(LGCIU)

32-31-01A A 2 1 (O)(FD) The LGCIU 2 may be inoperative for one flight day

provided that:

1) All ELACs, SECs, SFCCs, RAs, FACs, and ADIRSsare operative,


3) The FLEX Takeoff Mode is not used,

4) The operation of avionics equipment is time limited onground,

5) Reverser number 2 considered inoperative,

6) Both radio altimeter systems are operative, and

7) Both FCU channels are operative.



HYDRAULIC/LGCIU/SYS2

(121VU Q35) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL

The following table gives the consequences on the

systems affected when the LGCIU 2 is inoperative and

above mentioned C/B is pulled.


30 JUN 12MEL

A320/321MEL/CDL 01.32.23

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-31 Normal Extension and

Retraction


Control and

Interface Unit

(LGCIU)





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-31 Normal Extension

and Retraction


Control and

Interface Unit

(LGCIU)



12 FEB 12MEL

A320/321MEL/CDL 01.32.25

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-31 Normal Extension and

Retraction


Control and

Interface Unit

(LGCIU)


IN FLIGHT

- In the case of loss of the LGCIU 1:

AP and FD are lost.



Retracting System

32-31-02A C 1 0 (O) May be inoperative provided that the aircraft is operated in

accordance with the Flight Manual supplement for the

flight with landing gear down.


Refer to FCOM/PRO-SPO-25 Flight With Gear Down.

32-32 Proximity Detector

System

32-32-01 LGCIU 1 Proximity

Detector




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-02 LGCIU 2 RH L/G

Shock Absorber

Proximity Detector

32-32-02A A 1 0 (O)(M)

(FD)

May be inoperative for one flight provided that:

1) Both radio altimeters are operative, and

2) The other proximity detectors are operative, and

3) The origin of the failure is checked to be electrical.


GENERAL INFORMATION


30 JUN 12MEL

A320/321MEL/CDL 01.32.27

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-02 LGCIU 2 RH L/G

Shock Absorber

Proximity Detector



Refer to AMM 32-31-00-040-003



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-02 LGCIU 2 RH L/G

Shock Absorber

Proximity Detector

32-32-02B A 1 0 (FD) May be inoperative for one flight provided that the LGCIU

2 is considered inoperative.

Refer to Item 32-31-01 Landing Gear Control and InterfaceUnit (LGCIU)

32-32-03 LGCIU 2 LH L/G

Shock Absorber

Proximity Detector

32-32-03A A 1 0 (O)(M)

(FD)

May be inoperative for one flights provided that:

1) Both radio altimeters are operative, and




GENERAL INFORMATION


30 JUN 12MEL

A320/321MEL/CDL 01.32.29

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR





MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-03 LGCIU 2 LH L/G

Shock Absorber

Proximity Detector



Refer to AMM 32-31-00-040-003

32-32-03B A 1 0 (FD) May be inoperative for one flight provided that the LGCIU


Refer to MEL 32-31-01 Landing Gear Control and

Interface Unit (LGCIU)

30 JUN 12MEL

A320/321MEL/CDL 01.32.31

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-04 LGCIU 2 Nose L/G

Shock Absorber

Proximity Detector

32-32-04A Other proximity

detectors

operative

A 1 0 (O)(M)

(FD)

May be inoperative for 7 flights provided that:




GENERAL INFORMATION


Refer to AMM 32-31-00-040-003

32-32-04B LGCIU 2

considered

inoperative

A 1 0 (FD) May be inoperative for one flight provided that the LGCIU


Refer to Item 32-31-01 Landing Gear Control and Interface

Unit (LGCIU)



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-05 LGCIU 2 RH L/G

Down Lock

Proximity Detector


detectors

operative





GENERAL INFORMATION


Refer to AMM 32-31-00-040-003

32-32-05B LGCIU 2

considered

inoperative



Refer to Item 32-31-01 Landing Gear Control and InterfaceUnit (LGCIU)

30 JUN 12MEL

A320/321MEL/CDL 01.32.33

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-06 LGCIU 2 LH L/G

Down Lock

Proximity Detector


detectors

operative





GENERAL INFORMATION


Refer to AMM 32-31-00-040-003

32-32-06B LGCIU 2considered

inoperative

A 1 0 (FD) May be inoperative for one flight provided that the LGCIU2 is considered inoperative.


Unit (LGCIU)



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System


Down Lock

Proximity Detector


detectors

operative





GENERAL INFORMATION


Refer to AMM 32-31-00-040-003


inoperative



Unit (LGCIU)

30 JUN 12MEL

A320/321MEL/CDL 01.32.35

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-08 LGCIU 2 RH L/G

Up Lock Proximity

Detector


detectors

operative

A 1 0 (O)(M)

(FD)





GENERAL INFORMATION


Refer to AMM 32-31-00-040-003

32-32-08B LGCIU 2

considered

inoperative




Unit (LGCIU)



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-09 LGCIU 2 LH L/G

Up Lock Proximity

Detector


detectors

operative

A 1 0 (O)(M)

(FD)





GENERAL INFORMATION


Refer to AMM 32-31-00-040-003

32-32-09B LGCIU 2

considered

inoperative




Unit (LGCIU)

30 JUN 12MEL

A320/321MEL/CDL 01.32.37

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System


Up Lock Proximity

Detector


detectors

operative

A 1 0 (O)(M)

(FD)





GENERAL INFORMATION


Refer to AMM 32-31-00-040-003

32-32-10B LGCIU 2

considered

inoperative




Unit (LGCIU)



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-11 LGCIU 2 RH L/G

Doors Open

Proximity Detector


detectors

operative

A 1 0 (O)(M)

(FD)





Refer to Operating Procedures 32-32-08A LGCIU 2 RH

L/G Up Lock Proximity Detector


Refer to AMM 32-31-00-040-003

32-32-11B LGCIU 2

considered

inoperative




Unit (LGCIU)

32-32-12 LGCIU 2 LH L/G

Doors Open

Proximity Detector


detectors

operative

A 1 0 (O)(M)

(FD)





Refer to Operating Procedures 32-32-09A LGCIU 2 LH



Refer to AMM 32-31-00-040-003

30 JUN 12MEL

A320/321MEL/CDL 01.32.39

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-12 LGCIU 2 LH L/G

Doors Open

Proximity Detector

32-32-12B LGCIU 2

considered

inoperative




Unit (LGCIU)


Doors Open

Proximity Detector


detectors

operative

A 2 0 (O)(M)

(FD)

One or both may be inoperative for 7 flights provided that:




Refer to Operating Procedures 32-32-10A LGCIU 2 Nose



Refer to AMM 32-31-00-040-003


inoperative

A 2 0 (FD) One or both may be inoperative for one flight providedthat the LGCIU 2 is considered inoperative.


Unit (LGCIU)



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-14 LGCIU 2 RH L/G

Doors Closed

Proximity Detector


detectors

operative

A 1 0 (O)(M)

(FD)


1) The other proximity detectors are operative.



Refer to Operating Procedures 32-32-08A LGCIU 2 RH



Refer to AMM 32-31-00-040-003


inoperative



Unit (LGCIU)

30 JUN 12MEL

A320/321MEL/CDL 01.32.41

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System

32-32-15 LGCIU 2 LH L/G

Doors Closed

Proximity Detector


detectors

operative

A 1 0 (O)(M)

(FD)





Refer to Operating Procedures 32-32-09A LGCIU 2 LH



Refer to AMM 32-31-00-040-003


inoperative



Unit (LGCIU)



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


System


Doors Closed

Proximity Detector


detectors

operative

A 1 0 (O)(M)

(FD)





Refer to Operating Procedures 32-32-10A LGCIU 2 Nose



Refer to AMM 32-31-00-040-003

32-32-16B LGCIU 2

considered

inoperative




Unit (LGCIU)

32-33 Free Fall Extension


Gravity Extension

System

32-33-01A C 1 0 (O) May be inoperative provided that the aircraft is operated in

accordance with the Flight Manual supplement for the

flight with landing gear down.


Refer to FCOM/SPO-25 Flight With Gear Down.

30 JUN 12MEL

A320/321MEL/CDL 01.32.43

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-41 Wheels

32-41-01 Nose Wheel Tie

Bolt

32-41-01A A 12 11 (M)(FD) One tie bolt on one wheel may be broken or missing for 15

flights provided that:

1) The affected wheel tie bolt is removed, and

2) The affected wheel and the associated brake arechecked for absence of damage.


Refer to AMM 32-41-00-040-002

32-41-02 Main Wheel Tie

Bolt

32-41-02A A 18 17 (M)(FD) One tie bolt on one wheel may be broken or missing for 15

flights provided that:

1) The affected wheel tie bolt is removed, and

2) The affected wheel and the associated brake arechecked for absence of damage.


Refer to AMM 32-41-00-040-003



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-42 Normal Braking

32-42-01 Main Wheel Brake

32-42-01A C 4 3 (O)(M)

(FD)


1) The nose wheel steering is operative, and

2) Both thrust reversers are operative, and

3) The green and yellow systems are operative onoperative brakes, and

4) The affected brake is deactivated or removed, and

5) The runway width at departure and arrival airports is atleast 45 m, and

5) The Flight Manual performance penalties areapplied,and

6) Anti-skid system is operative and Wheel tachometers

are operative.


30 JUN 12MEL

A320/321MEL/CDL 01.32.45

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR






For performance calculations request Modified TailoredTakeoff and Landing charts (MTTL) from FPE through

Flight Dispatch.



FOR TAKEOFF

The autobrake function, even if available, must not be

used.


-- In the case of engine failure at takeoff:Retract the landing gear when positive climb.

Vibrations may occur during 1 or 2 min after theretraction of the landing gear.

- If both engines are operative:

Keep the landing gear down for 1 min.

FOR LANDING


used.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR






Flight Dispatch.



FOR TAKEOFF


used.


- In the case of engine failure at takeoff:

Retract the landing gear when positive climb.Vibrations may occur during 1 or 2 min after theretraction of the landing gear.

- If both engines are operative:

Keep the landing gear down for 1 min.

FOR LANDING

The autobrake function, even if available, must not beused.


Refer to AMM 32-42-00-040-003

30 JUN 12MEL

A320/321MEL/CDL 01.32.47

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


32-42-02 Green System

Brake

32-42-02A C 1 1 (O)(M)(FD)

Braking on one wheel may be inoperative provided that:1) The nose wheel steering is operative, and


3) The green hydraulic supply of affected brake isdeactivated, and

4) The runway width at departure and arrival airports is atleast 45 m, and



Refer to Operating Procedures 32-42-01A Main Wheel

Brake


Refer to AMM 32-42-00-040-002



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


32-42-03 Braking/Steering

Control Unit

(BSCU) System 1


1) The BSCU system 2 is operative, and

2) The affected system is deactivated, and

3) It is checked that the CFDS does not report a faultrelated to the L/G SYS DISAGREE alert before eachflight, and

4) The AUTO/BRK (LO, MED, MAX) pb-sw DECEL lightand the AUTO/BRK (LO, MED, MAX) pb-sw ON lightare considered inoperative, and

5) Brake pressure indicators is operative, and

6) Alternate brake system checked operative before eachdepature.

Refer to Item 32-42-08 AUTO/BRK (LO, MED, MAX) pb-sw DECEL light, and

Refer to Item 32-42-09 AUTO/BRK (LO, MED, MAX) pb-sw ON light


Refer to AMM 32-42-00-040-007


Control Unit

(BSCU) System 2


1) The affected system is deactivated, and

2) It is checked that the CFDS does not report a faultrelated to the L/G SYS DISAGREE alert before eachflight, and


30 JUN 12MEL

A320/321MEL/CDL 01.32.49

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR



Control Unit

(BSCU) System 2

32-42-04A (Cont’d) 3) Brake pressure indicators is operative, and

4) Alternate brake system checked operative before eachdepature.


Refer to AMM 32-42-00-040-007

32-42-05 AUTO/BRK

Function





BEFORE TAKEOFF

When T.O MEMO is displayed on the EWD, disregard the

line:

AUTO BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX (blue)

32-42-06 Tachometer

32-42-06B 4 4 Must be operative.

32-42-08 AUTO/BRK (LO,

MED, MAX) pb-sw

DECEL light




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


32-42-09 AUTO/BRK (LO,

MED, MAX) pb-sw

ON light

32-42-09A AUTO/BRK

mode arming

displayed on

the WHEEL SD

page

C 3 0 One or more may be inoperative provided that, when

appropriate, the associated AUTO/BRK mode arming is

displayed on the WHEEL SD page.

32-42-09B AUTO/BRK

function

considered

inoperative


AUTO/BRK function is considered inoperative.

Refer to Item 32-42-05 AUTO/BRK Function

32-44 Alternate Braking


Brake

32-44-01A C 1 1 (M) Braking on one wheel may be inoperative provided that:


2) The yellow hydraulic supply of the affected brake isdeactivated.


Refer to AMM 32-43-00-040-001

30 JUN 12MEL

A320/321MEL/CDL 01.32.51

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-44 Alternate Braking

32-44-02 ACCU PRESS

Indicator

32-44-02A Brakes

pressure

indicator

operative


1) Both brakes pressure indicators are operative, and

2) The pressure on both brakes pressure indicators ischecked with parking brake ON before each flight.

32-44-02B Checks on

WHEEL SD

page


1) The ACCU PRESS/ACCU ONLY indication isoperative on the WHEEL SD page, and

2) The hydraulic pressure of the brake accumulator ischecked on the WHEEL SD page before each flight.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR


32-44-03 BRAKES Pressure

Indicator

32-44-03A C 2 0 One or both may be inoperative provided that the BSCU

system 1 and the BSCU system 2 are operative.

32-44-04 Alternate Braking

Control Unit

(ABCU)


32-45 Parking/Ultimate

Emergency Braking

32-45-01 Parking Brake

Control Valve

Electrical Motor



2) The aircraft is not towed if the STBY motor is affectedand when the batteries supply the aircraft.


Refer to AMM 32-45-00-040-001

30 JUN 12MEL

A320/321MEL/CDL 01.32.53

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-47 Brake Temperature

System

32-47-01 Brake

Temperature

Monitoring Unit

(BTMU)

32-47-01A C 2 0 (O) One or both may be inoperative provided that the ground

brake cooling time is applied.



HYDRAULIC/BRK/TEMP/DET/UNIT

(121VU M26 or M37) C/B. . . . . . . . . . . . . . . . . . . . . . PULL

Determine brake cooling time (Refer to OpsProc 32-07-

01A(B) Brakes Temperature Indication on the WHEEL SD

page).

32-48 Brake Cooling

32-48-01 Brake Fan System


32-48-02 BRK FAN pb-sw

HOT light


32-48-03 BRK FAN pb-sw

ON light


Note:

Brake Fan operation may be checked through the brake

fan ECAM MEMO.



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-51 Steering

32-51-01 Nose Wheel

Steering Control

System

32-51-01A A 1 1 Must be operative.

32-51-02 Rudder PEDALS

DISC pb

32-51-02A C 2 0 (O) One or both may be inoperative (no disconnection is

possible).


The purpose of the procedure is to explain how to perform

the flight control check with one or both PEDALS DISC pb

failed in the released position.


GENERAL INFORMATION

- When the disconnection is not possible on oneside:The flight control check can be performed on theoperative side.

- When the disconnection is not possible on bothsides:The flight control check must be performed whileaircraft is stopped.

Note:

It is not necessary to set the A/SKID &N/W STRG sw to OFF.

30 JUN 12MEL

A320/321MEL/CDL 01.32.55

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-51 Steering

32-51-03 NWS Electrical

Deactivation Box

32-51-03A No towing

mode when

lever in the

TOWING

position

C 1 0 (O) May be inoperative.

Note:

The towing mode is not available when

the lever is in the TOWING position.


BEFORE CONVENTIONAL OR TOWLESS PUSHBACK

A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . OFF

AFTER PUSHBACK

A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . . ON

32-51-03B NWS electrical

deactivation

box deactivated

C 1 0 (O)(M) May be inoperative provided that the NWS electrical

deactivation box is deactivated.




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-51 Steering

32-51-03 NWS Electrical

Deactivation Box

32-51-03B NWS electrical

deactivation

box deactivated

(Cont’d)


BEFORE CONVENTIONAL OR TOWLESS PUSHBACK

A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . OFF

As a result of the NWS electrical box deactivation, the

parking brake light on that box will not be available.

The parking brake setting must be verbally confirmed

between the flight crew and the ground personnel before

pushback.

AFTER PUSHBACK

A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . . ON


Refer to AMM 32-51-00-040-002

30 JUN 12MEL

A320/321MEL/CDL 01.32.57

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-51 Steering

32-51-04 PARKING BRAKE

light on the NWS

Electrical

Deactivation Box



BEFORE PUSHBACK

The parking brake setting must be verbally confirmed

between the flight crew and the ground personnel.

32-61 Landing Gear Panel

on the Center

Instrument Panel

32-61-01 LDG GEAR

Indicator Panel


32-61-02 DOWN Red Arrow

light on the

Landing Gear

lever

32-61-02A C 1 0 (M) May be inoperative provided that the L/G GEAR NOT

DOWN alert and the L/G GEAR NOT DOWNLOCKED

alert are checked operative.


Refer to AMM 32-61-00-040-001

* * *



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



MEL

A320/321MEL/CDL 01.32.59

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



A320/321MEL/CDL

MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


MEL

A320/321MEL/CDL 01.32.61

LANDING GEAR



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


12 FEB 12MEL

A320/321MEL/CDL 01.32.63

LANDING GEAR



SEQUENCE


D

I T E M

7/23/2019 A 320321 Mel Cdl



A320/321MEL/CDL

MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS


33-01-01 ANN LT

Overhead Panel

33-01-01-01 TEST Function

of ANN LT sw


33-01-01-02 DIM Function of

ANN LT sw

33-01-01-02A C 1 0 Dim lighting may be inoperative provided that the bright

lighting is operative.

33-01-01-03 BRT Function of

ANN LT sw

33-01-01-03A C 1 0 Bright lighting may be inoperative for night operation.

33-01-02-01 EMER EXIT LT

OFF light

33-01-02-01A C 1 0 (M) May be inoperative provided that the emergency lighting

system is checked operative every day.


Refer to AMM 33-51-00-040-002

12 FEB 12MEL

A320/321MEL/CDL 01.33.01

LIGHTS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS


33-01-01 ANN LT

Overhead Panel

33-01-02-02 AUTO Function

of SEAT BELT

SIGNS sw




SEAT BELTS selector · · · · · · · · · · · · · · · · · · · · · · · ON

AFTER TAKEOFF

SEAT BELTS selector · · · · · · · · · · · · · · · · As required

DURING APPROACH

SEAT BELTS selector · · · · · · · · · · · · · · · · · · · · · · · ON

33-01-02-03 AUTO Function

of NO SMOKING

SIGNS sw




Check that the passenger address function isoperative in the affected lavatory with the door closed.

01.33.02LIGHTS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-10 Cockpit General

Illumination

33-10-01 Cockpit General

Illumination

(Center & Main

Instrument

Lighting,

Console and

Floor Lighting,

Dome lights and

Lighting Strips,

Instrument and

Panel Integral

Lighting, Map

Holder Lighting,

Center Pedestal

Lighting)


1) The lighting is sufficient for all instruments andcontrols, and

2) The RH dome light is operative, and

3) The left section of the center main panel flood light isoperative.

NOTE: RH dome light is considered operative with a

minimum of three bulbs illuminated in each assembly. The

bulbs can be checked by selecting the DOME toggle

switch from DIM to BRT and ensure both functions

operate.

33-20 Cabin General

Illumination

33-20-01 Cabin General

Illumination

33-20-01A C 6 3 The lighting must be sufficient for cabin attendants to

perform their duties.

30 JUN 12MEL

A320/321MEL/CDL 01.33.03

LIGHTS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-20 Cabin General

Illumination

33-20-02 Cabin Signs (No

Smoking/No

Electronic

Devices/Fasten

Seat Belt/Return

to Seat)

33-20-02A Passenger seat

occupied

C 30 0 One or more may be inoperative and the affected

passenger seat may be occupied provided that:

1) The passenger address system is operative, and canbe heard throughout the cabin during the flight, and

2) The passenger address system is used to alert thepassengers when return to seat is requested, seatbelts should be fastened and smoking is prohibited.

33-20-02B Passenger seat

not occupied

C 30 0 (M)(FD)One or more “No Smoking/Fasten Seat Belt” sign may be


1) No passenger seat is occupied from which a

passenger cannot see a readily legible “Nosmoking/Fasten Seat Belt” sign, and

2) The affected seat is blocked and placardedinoperative.


Refer to AMM 33-20-00-040-001

01.33.04LIGHTS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-20 Cabin General

Illumination

33-20-03 Lavatory Sign

(Return to seat)

33-20-03A C 3 0 (O)(FD) One or more may be inoperative and the affected lavatory

may be used provided that:

1) The passenger address system is checked operative

in the affected lavatory, and2) The passenger address system is used to alert the

occupant to return to his seat.



Check that the passenger address function is operative in

the affected lavatory with the door closed.

12 FEB 12MEL

A320/321MEL/CDL 01.33.05

LIGHTS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-30 Cargo and Service

Compartment Lighting

33-30-01 Cargo and

Service

Compartment

Lighting System


33-40 Exterior Lighting

33-40-01 Navigation light

System 1

33-40-01A Daylight

operations

C 3 0 (FD) One or more may be inoperative for daylight operations.

33-40-01B Navigation light

system 2

operative


Navigation light system 2 is operative.

33-40-02 Navigation lightSystem 2


33-40-03 Landing light

33-40-03A Nose, taxi and

takeoff lights

operative

C 2 1 One may be inoperative provided that the nose, taxi and

takeoff lights are operative.

33-40-03B Daylight

operations

C 2 0 (FD) One or both may be inoperative for daylight operations.

01.33.06LIGHTS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS


33-40-04 Landing light

Extension/

Retraction

System


extended

position

C 2 0 (O)(FD) One or both may be inoperative in the extended position.



The fuel consumption is increased by 1 % per landing light

extended.


retracted

position

C 2 0 One or both may be inoperative in the retracted position

provided that the associated light is considered

inoperative.

Refer to MEL Item 33-40-03 Landing light

33-40-05 Runway Turnoff

lights


33-40-06 Taxi and Takeoff

light


33-40-07 Logo lights

33-40-07A D 2 0 One or both may be inoperative.

30 JUN 12MEL

A320/321MEL/CDL 01.33.07

LIGHTS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS


33-40-08 Beacon light

33-40-08A Daylight

operations

C 2 0 (O)(FD) One or both may be inoperative for daylight operations.


BEFORE ENGINE START

- If the bottom light is inoperative:

If this light is used to alert the ground crew of theengine start, the captain must brief the groundmechanic regarding beacon light.

33-40-08B Strobe lights

operative

C 2 0 (O) One or both may be inoperative provided that the Strobe

lights are operative.



33-40-09 Wing Scan lights

33-40-09A Daylight

operations

C 2 0 (FD) One or both may be inoperative for daylight operations.

33-40-09B Night

operations

C 2 1 One may be inoperative for night operations.

33-40-10 Strobe light


01.33.08LIGHTS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-51 Cabin Emergency

Lighting

33-51-01 Exit Marking

Sign

(A320)

33-51-01B A maximum of

three non-

adjacent LEDs

inoperative

C 6 6 A maximum of three non-adjacent LEDs may be

inoperative in one or more signs.

33-51-01 Exit Marking

Sign

(A321)

33-51-01B A maximum of

three non-

adjacent LEDs

inoperative

C 8 8 A maximum of three non-adjacent LEDs may be


33-51-02 Exit Location

Sign in the MainAisle

33-51-02A C 18 15 A maximum of three non-adjacent LEDs may be


33-51-03 Overhead

Emergency

Lighting System

in the Main Aisle

33-51-03A C 22 19 A maximum of three non-adjacent overhead emergency

lights may be inoperative.

12 FEB 12MEL

A320/321MEL/CDL 01.33.09

LIGHTS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS


Lighting

33-51-04 Overhead

Emergency

Lighting System

in the Door

Vicinity

(A320)

33-51-04A Refer to Item 52-10-01 Cabin Passenger Door, and

Refer to Item 52-10-02 Overwing Emergency Exit

33-51-04 Overhead

Emergency

Lighting System

in the Door

Vicinity

(A321)

33-51-04A Refer to MEL Item 52-10-01 Cabin Passenger Door

33-51-05 Floor Proximity

Emergency

Escape Path

Marking System

in the Main Aisle

33-51-05A

( M : meters )

C 80

M

79

M

Each of the photoluminescent strips of an aisle may be

inoperative or missing up to a length of 0,25 meter

(10 inches) provided the inoperative or missing parts are

not directly opposite each other and are not closer than 2,0

meter (78.74 inches). No more than four such inoperative

or missing parts are allowed provided:

1- All strips within 1 meter of an exit is operative, and

2- All strips marking right angle intersection includingcross aisles and overwing exits are operative.

01.33.10LIGHTS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


33 LIGHTS


Lighting

33-51-07 Floor Proximity

Emergency

Escape Path

Marking System

Exit Marker

33-51-07A Refer to MEL Item 52-10-01 Cabin Passenger Door, and

Refer to MEL Item 52-10-02 Overwing Emergency Exit

33-51-08 Overwing

Emergency light

33-51-08A Daylight

operations

C 4 0 (FD) One or more may be inoperative for daylight operations.


Lighting

33-51-09 Overwing ExitHandle light


33-51-10 Escape Slide

Lighting

33-51-10A Daylight

operations

C 8 0 May be inoperative for daylight operations.

33-51-11 LavatoryAuxiliary light


* * *

12 FEB 12MEL

A320/321MEL/CDL 01.33.11

LIGHTS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl





SEQUENCE


I T E MI T E M



SEQUENCE


01.33.12LIGHTS


MEL

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-00 MAINTENANCE

Messages on the

STATUS SD page

34-00-01 ADR (1)(2)(3)

MAINTENANCE

Message

34-00-01A C 3 - ADR (1)(2)(3) MAINTENANCE message may be displayed


34-00-02 IR

MAINTENANCE

Message

34-00-02A C 3 - IR MAINTENANCE message may be displayed on the

STATUS SD page.

34-01 Overhead

Panels

34-01-01 ADIRS

Overhead Panel

34-01-01-01 ADR pb-sw

FAULT light


34-01-01-02 ADR pb-sw OFF

light


34-01-01-03 IR pb-sw FAULT

light


34-01-01-04 IR pb-sw OFF

light


12 FEB 12MEL

A320/321MEL/CDL 01.34.01

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


34-01-01 ADIRS Overhead

Panel

34-01-01-04 IR pb-sw OFF

light


34-01-01-05 ON BAT light


34-01-01-31 ADR pb-sw

34-01-01-31A C 3 2 (O) ADR 2 or ADR 3 pb-sw may be inoperative provided that:

1) The associated mode selector is operative, and

2) The two ADRs and the two IRs associated with the twooperative ADRs pb-sw are operative.


IN FLIGHT

If needed, the associated ADR can be set to OFF through

the associated mode selector.

Note:

- If the ADR is set to OFF:

The associated IR is also set to OFF.

The F/CTL MAINTENANCE message is


01.34.02NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


34-01-01 ADIRS Overhead

Panel

34-01-01-32 IR pb-sw

34-01-01-32A C 3 2 (O) IR 2 or IR 3 pb-sw may be inoperative provided that:

1) The associated mode selector is operative, and

2) The two ADRs and the two IRs associated with the twooperative IRs pb-sw are operative.


FLIGHT

If needed, the associated IR can be set to OFF through the

associated mode selector.

Note:

- If the IR is set to OFF:

The associated ADR is also set to

OFF.

The F/CTL MAINTENANCE

message is displayed on the

STATUS SD page.

34-01-01-33 IR Mode selector


12 FEB 12MEL

A320/321MEL/CDL 01.34.03

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


34-01-02 GPWS Overhead

Panel

34-01-02-01 GPWS SYS

FAULT light

34-01-02-01A C 1 0 May be inoperative provided GPWS is verified operative

before each departure.



(PFD)

34-05-01 Actual Airspeed

Reference Line

and Scale

Indication on the

PFD


34-05-02 Mach Number

Indication on the

PFD

34-05-02A One indication

inoperative

C 2 1 One may be inoperative.

34-05-02B Both indications

inoperative - FCU

operative

C 2 0 Both may be inoperative provided that the SPD/MACH

selection window on the FCU is operative.

34-05-02C Both indications

inoperative - FLlimitation

C 2 0 (FD) Both may be inoperative provided that the flight altitude is

limited to 25 000 ft.

34-05-02D Both indications

inoperative - ISIS

Mach Number

Function operative

C 2 0 Both may be inoperative provided that the ISIS Mach

Number indication is operative.

01.34.04NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Primary Flight

Display (PFD)

34-05-03 VMO/MMO

Characteristic

Speed Indication

on the PFD


34-05-04 Altitude

Indication on the

PFD


34-05-05 Baro Reference

Indication on the

PFD

34-05-05A 2 2 Both must be inoperative.

34-05-06 Vertical Speed in

Inertial Mode

Indication on the

PFD


12 FEB 12MEL

A320/321MEL/CDL 01.34.05

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION



(PFD)

34-05-07 Other Air Data

Related

Indications on the

PFD



GENERAL INFORMATION

For F, S, Green Dot determination, refer to the QRH/FPE-

SPD speeds.

For VAPP determination, refer to QRH/FPE-IFL-VAPP

determination.

For VFE or VLE determination, refer to the corresponding

placard in the cockpit.

34-05-08 Attitude Indication

on the PFD

34-05-08A C 2 1 (O) One may be inoperative provided that the aircraft is

operated in day VMC conditions.





on the PFD


01.34.06NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Navigation Display

(ND)

34-06-01 Ground Speed

Indication on the

ND


34-06-02 True Air Speed

Indication on the

ND


34-06-03 Wind Indication

on the ND


34-06-04 Heading

Indication on theND

34-06-04A C 2 1 One may be inoperative provided that the heading

indications are operative on both PFDs.

34-06-05 Position

(Aircraft

Symbol)

Indication on the

ND


34-06-06 Radio Navaids

Indications on

the ND


12 FEB 12MEL

A320/321MEL/CDL 01.34.07

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Navigation Display

(ND)

34-06-07 Chrono Indication

on the ND


34-10 Air Data/Inertial

Reference System

(ADIRS)

34-10-01 ADR 1


34-10-02 ADR 2


1) The IR 1, IR 3, ADR 1 and ADR 3 are operative, and

2) The takeoff is not performed in CONF 1+F.





- ADR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF

The F/CTL MAINTENANCE message is displayed onthe STATUS SD page.

- AIR DATA SWITCHING selector · · · · · · · · · · · · · F/O 3

- ADIRS/ADIRU/2/26VAC AND AOA(location 121VU N08 or N09) C/B · · · · · · · · · · · · · Pull


01.34.08NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Reference System

(ADIRS)

34-10-02 ADR 2


AFTER ENGINE START

- Use the RCL pb-sw on the ECAM control panel, inorder to recall the NAV ADR 2 FAULT alert.

- On the EWD, check that the ADR 2...OFF procedure isnot displayed.

FOR TAKEOFF

Takeoff in CONF 1+F is not permitted.

Note:

When the ADR 2 pb-sw is set to OFF,

and if the aircraft is in CONF 1+F, the

SFCS n°2 Flap channel is unable to

crosscheck the airspeed coming fromthe ADR 1 with the ADR 2 airspeed

coming from the SFCS n°2 Slat channel.

This may lead to an uncommanded flap

retraction during the takeoff. As a

consequence, takeoff in CONF 1+F is

not permitted when the ADR 2 pb-sw is

set to OFF.

12 FEB 12MEL

A320/321MEL/CDL 01.34.09

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Reference System

(ADIRS)

34-10-03 ADR 3

34-10-03A C 1 0 (O) May be inoperative provided that the IR 1, IR 2, ADR 1

and ADR 2 are operative.





- ADR 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF


- ADIRS/ADIRU/3/26VAC AND AOA(location 121VU N07 or N08) C/B· · · · · · · · · · · · · · Pull

AFTER ENGINE START

- Use the RCL pb-sw on the ECAM control panel, inorder to recall the NAV ADR 3 FAULT alert.

- On the EWD, check that the ADR 3...OFF procedure isnot displayed.

01.34.10NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Reference System

(ADIRS)

34-10-04 IR 1

34-10-04B GPS 1

operative

B 1 1 (O)(FD) The NAV mode may be inoperative provided that:

1) The IR 1 is operated in ATT mode, and

2) The IR 2 and IR 3 are operative, and

3) The GPS 1 is operative, and

4) The terrain function of the TAWS is consideredinoperative.Refer to MEL Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS)





- ATT HDG SWITCHING selector · · · · · · · · · · · CAPT 3

- IR 1 mode selector· · · · · · · · · · · · · · · · · · · · · · · · · ATT

- The heading must be entered through the MCDU for the IR 1 and has to be frequently reset(Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN

ATT MODE).

34-10-04C GPS 1

inoperative

B 1 1 (O)(FD) The NAV mode may be inoperative provided that:


2) The IR 2 and IR 3 are operative, and

3) The Flight remains within radio navaids coverage, and

4) The terrain function of the TAWS ñ– is consideredinoperative.Refer to MEL Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS)


12 FEB 12MEL

A320/321MEL/CDL 01.34.11

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Reference System

(ADIRS)

34-10-04 IR 1

34-10-04C GPS 1 inoperative

(Cont’d)


Refer to MEL item 34-10-04B Operating Procedures

34-10-05 IR 2

34-10-05B IR 2 totally

inoperative


1) The IR 2 pb-sw is set to OFF, and

2) The IR 1, the IR 3, the ADR 1 and the two ADRs areoperative.





- IR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF


- ATT HDG SWITCHING selector · · · · · · · · · · · · · F/O 3

- AIR DATA SWITCHING selector · · · · · · · · · · · · · F/O 3

34-10-05C Only NAV mode of

IR 2 inoperative

C 1 0 (O) The NAV mode may be inoperative provided that:


2) The IR 1 and the IR 3 are operative.





01.34.12NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Reference System

(ADIRS)

34-10-05 IR 2

34-10-05C Only NAV mode

of IR 2

inoperative

(Cont’d)



- ATT HDG SWITCHING selector · · · · · · · · · · · · · F/O 3


- The heading must be entered through the MCDUkeyboard for the IR 2 and has to be frequently reset(Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN

ATT MODE).

34-10-07 IR 3

34-10-07A IR 3 mode

selector set to

OFF

B 1 0 (O) May be inoperative provided that:

1) The IR 3 pb-sw is set to OFF, and

2) The IR 1, the IR 2, the ADR 1, and the ADR 2 are

operative.


GENERAL INFORMATION

For aircraft fitted with Honeywell 10 MCU ADIRU,

disregard the characteristic speeds (Vls, F, S, Green Dot)

displayed on the PFD. For characteristic speeds (Vls, F, S,

Green Dot) determination, refer to the QRH. The “CHECK

GW” (or “CHECK WEIGHT”) message may be displayed

on the MCDU.




IR 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

The F/CTL MAINTENANCE message is displayed on the

STATUS SD page.

01 MAY 12MEL

A320/321MEL/CDL 01.34.13

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Reference System

(ADIRS)

34-10-07 IR 3

34-10-07B IR 3 operated in

ATT mode

C 1 0 (O) The NAV mode may be inoperative provided that:


2) The IR 1 and the IR 2 are operative.






- The heading must be entered through the MCDU for the IR 3 and has to be frequently reset.(Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN

ATT MODE).

34-11 Sensors


(AOA) Sensor

34-11-01A C 3 2 The F/O or the STBY Angle Of Attack sensor may be

inoperative provided that the associated ADR is


Refer to MEL Item 34-10-02 ADR 2, or

Refer to MEL Item 34-10-03 ADR 3

01.34.14NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-11 Sensors

34-11-02 CAPT Total Air

Temperature

(TAT) Sensor

Element

Connected to

ADR1


1) The CAPT sensor element connected to the ADR 3 isoperative, and

2) The F/O sensor connected to the ADR 2 is operative,and

3) The ADR 2 and the ADR 3 are operative, and

4) The TAT indication on the SD is checked operative,and

5) The TAS indication on the ND 1 is consideredinoperative.Refer to MEL Item 34-06-02 True Air Speed Indicationon the ND


Refer to Operating Procedures 31-07-02A Permanent

Data Indications on the SD

12 FEB 12MEL

A320/321MEL/CDL 01.34.15

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-11 Sensors

34-11-03 CAPT Total Air

Temperature (TAT)

Sensor Element

Connected to

ADR3


1) The CAPT sensor element connected to the ADR 1 isoperative, and

2) The F/O sensor connected to the ADR 2 is operative,and


4) The TAT indication on the SD is checked operative.



Check that the TAT is displayed on the SD permanent

data.

34-11-04 F/O Total Air

Temperature (TAT)

Sensor Element

Connected to

ADR2


1) Both CAPT TAT sensor elements are operative, and


3) The TAT indication on the SD is checked operative,and

4) The TAS indications on the ND 2 is consideredinoperative.Refer to MEL Item 34-06-02 True Air Speed Indicationon the ND


01.34.16NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-11 Sensors

34-11-04 F/O Total Air

Temperature

(TAT) Sensor

Element

Connected to

ADR2


Refer to Operating Procedures 31-07-02A Permanent

Data Indications on the SD

34-21 Altitude and

Airspeed Standby

Data

34-21-05 Standby ALT

Metric Indicator


12 FEB 12MEL

A320/321MEL/CDL 01.34.17

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-22 Attitude and Heading

Standby Data

34-22-01 Standby Compass

Indicator

34-22-01A Applicable to

aircraft fitted with

NORTHROP

GRUMMAN

(LITTON) ADIRU

except P/N 465020-

0303-0316 or

subsequent, having

the shelf modified

(MOD 30650/SB

25-1248, or MOD

30872)

1 1 Must be operative.

34-22-01B Applicable to


NORTHROP

GRUMMAN(LITTON) ADIRU

P/N 465020-0303-

0316 or

subsequent, having

the shelf modified

(MOD 30650/SB

25-1248, or MOD

30872) or

HONEYWELL

ADIRU


1) The three IRs are operative, and

2) The ATT/HDG SWITCHING selector, the EIS DMCSWITCHING selector and the PFD/ND XFR pb arechecked operative.



Check of the ATT HDG, PFD/ND, and EIS DMCswitching:

- ATT HDG SWITCHING selector . . . . . . . . CAPT 3

- Check that the display is normal on the CAPT

PFD, the CAPT ND, and the RMI VOR.

- ATT HDG SWITCHING selector . . . . . . . . . . F/O 3

- Check that the display is normal on the F/O PFD

and the F/O ND.

- ATT HDG SWITCHING selector . . . . . . . . . NORM

- EIS DMC SWITCHING selector. . . . . . . . . CAPT 3

- Check that the display is normal on the CAPT PFD

and the CAPT ND.


01.34.18NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-22 Attitude and

Heading Standby

Data

34-22-01 Standby

Compass

Indicator

34-22-01B Applicable to


NORTHROP

GRUMMAN

(LITTON) ADIRU

P/N 465020-0303-

0316 or

subsequent, having

the shelf modified

(MOD 30650/SB

25-1248, or MOD

30872) or

HONEYWELL

ADIRU


- EIS DMC SWITCHING selector . . . . . . . . . . F/O 3

- Check that the display is normal on the F/O PFD

and the F/O ND.

- EIS DMC SWITCHING selector . . . . . . . . . NORM

- CAPT PFD/ND XFR pb . . . . . . . . . . . . . . . . . Press

- Check that the CAPT PFD and the CAPT ND

images are exchanged.

- CAPT PFD/ND XFR pb . . . . . . . . . . . . . . . . . Press

- F/O PFD/ND XFR pb. . . . . . . . . . . . . . . . . . . Press

- Check that the F/O PFD and the F/O ND images

are exchanged.

- F/O PFD/ND XFR pb. . . . . . . . . . . . . . . . . . . Press

34-22-02 Standby

Compass

Lighting


12 FEB 12MEL

A320/321MEL/CDL 01.34.19

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-23 Integrated Standby

Instrument System

(ISIS)

34-23-01 ISIS Baro-Altitude

Indication

34-23-01A B 1 0 May be inoperative provided that the aircraft is operated in

day VMC conditions.

34-23-02 ISIS Airspeed

Indication


1) The ISIS attitude indication is operative, and

2) The ADRs, DMCs and probe heat computers areoperative, and

3) The AIR DATA SWITCHING selector, the EIS DMCSWITCHING selector and the PFD/ND XFR pb areoperative.

34-23-03 ISIS BugsIndication


01.34.20NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-23 Integrated

Standby

Instrument

System (ISIS)

34-23-04 ISIS Attitude

Indication

34-23-04B B 1 0 (O)(FD) M ay be inoperative provided that the aircraft is operated in

day VMC conditions.




12 FEB 12MEL

A320/321MEL/CDL 01.34.21

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-23 Integrated Standby

Instrument System

(ISIS)

34-23-05 ISIS ILS Indication


34-23-06 ISIS Mach Number

Indication


34-30 Landing and Taxiing

Aid

34-30-04 Instrument

Landing System

(ILS)

34-30-04A C 2 1 (O)(FD) One ILS may be inoperative for VMC operations or for IMC

operations provided approach minimums do not require

use.

Note:

When the ILS 1 is inoperative, the

reactive modes of TAWS are

inoperative. Refer to Item 34-40-01

Ground Proximity Warning System

(GPWS)/Terrain Awareness and

Warning System (TAWS)


01.34.22NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-30 Landing and

Taxiing Aid

34-30-04 Instrument

Landing System

(ILS)


Note:

- When one ILS is inoperative:

Maximum landing capability is ILS CAT I.

- When both ILS are inoperative:

CAT I ILS approaches are not permitted.

34-40 GPWS/TAWS,

Radio Altimeter,

TCAS, Weather

Radar

34-40-01 Ground

Proximity

Warning System

(GPWS)/Terrain

Awareness and

Warning System

(TAWS)

34-40-01A A 1 0 (O) May be inoperative provided:

a) For the intent of returning International Flights toeither JED, RUH or DMM, the aircraft may continuethe flight sector(s) scheduled before the failure,

b) Flight is conducted under Day VMC conditions,and

c) Repairs are made within one flight day.


12 FEB 12MEL

A320/321MEL/CDL 01.34.23

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-40 GPWS/TAWS, Radio

Altimeter, TCAS,

Weather Radar

34-40-01 Ground Proximity

Warning System

(GPWS)/Terrain

Awareness and

Warning System

(TAWS)


Flight crew should increase their awareness of airplane

configuration, altitude and flight path at all times and

review and comply with Minimum Enroute Altitudes (MEA)

and altitude callouts.

34-40-01B Modes 1- 4 A 4 0 (O) May be inoperative provided:

1) For the intent of returning International Flights toeither JED, RUH or DMM, the aircraft may continuethe flight sector(s) scheduled before the failure,

2) Flight is conducted under Day VMC conditions,and

3) Repairs are made within one flight day.






34-40-01C Test Mode A 1 0 (O) May be inoperative provided:

1) For the intent of returning International Flights to

either JED, RUH or DMM, the aircraft may continuethe flight sector(s) scheduled before the failure,

2) Flight is conducted under Day VMC conditions,and

3) Repairs are made within one flight day.


01.34.24NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-40 GPWS/TAWS,

Radio Altimeter,

TCAS, Weather

Radar

34-40-01 Ground

Proximity

Warning System

(GPWS)/Terrain

Awareness and

Warning System

(TAWS)

34-40-01C Test Mode

(Cont’d)






34-40-01D Glideslope

Deviation Mode

5

B 1 0 May be inoperative.

34-40-01E Advisory Call-

Outs

C 7 0 (O) May be inoperative provided alternate procedures are

established and used.


The PM must be briefed to handle all the advisory calls per

FCOM instructions.

34-40-01F TAWS C 1 0 (O) May be inoperative provided alternate procedures are





comply with Minimum Enroute Altitude (MEA).

12 FEB 12MEL

A320/321MEL/CDL 01.34.25

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Altimeter, TCAS,

Weather Radar

34-40-02 Radio Altimeter

Automatic Callout




Maximum Landing capability is CAT I.


System

30-40-03A C 2 1 (O) One may be inoperative provided that both FCU channels,

all ELACs, SECs, ADIRUs, SFCCs, LGCIUs and FACs are

operative.

Note:

When the radio altimeter 1 is

inoperative, the reactive modes of

TAWS are inoperative.

Refer to MEL 34-40-01 Ground

Proximity Warning System


Warning System.


FLIGHT PREPERATION LIMITATION

Maximum landing Capability is CAT I.

The F/CTL MAINTENACE Message is displayed on the

STATUS SD page.


01.34.26NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-40 GPWS/TAWS,

Radio Altimeter,

TCAS, Weather

Radar


System


DURING COCKPIT PREPERATION

< If RA 1 is inoperative:

COM NAV/RAD ALTM/1 (121VU K11) C/B. . . . . . . . . . Pull

< If RA 2 is inoperative:

COM NAV/RAD ALTM/2 (121VU K12) C/B. . . . . . . . . . Pull

34-40-04 Traffic Collision

Avoidance

System (TCAS)


Note:

When the TCAS is deactivated, the

TAWS is also inoperative.

Refer to Item 34-40-01 Ground

Proximity Warning System


Warning System (TAWS)

34-40-05 Weather Radar

System


30 JUN 12MEL

A320/321MEL/CDL 01.34.27

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION


Altimeter, TCAS,

Weather Radar

34-40-05 Weather Radar

System

34-40-05B B 2 0 (FD) Both may be inoperative provided:

1) Flight is conducted in Day VMC, and

2) For IMC or Night VMC flights, provided currentweather reports do not indicate any thunderstorms or other potentially hazardous weather conditions whichcan be detected by weather radar.

Note:

When the captain and flight dispatcher

have determined that weather radar

inoperative requirements are met, the

associated Dispatch Release must

include the following statement:“Airborne weather radar is inoperative

and not required.”

Note:

When the weather radar system is

inoperative, the predictive Windshear

Detection System is inoperative .

Refer to Item 34-40-06 Weather

Radar/Predictive Windshear Detection

Function .

01.34.28NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-40-06 Predictive

Windshear

Detection

Function

34-40-06A Refer to MEL item 22-60-03A

34-40-07 PULL UP-GPWS

pb-sw

34-40-07A One

inoperative

C 2 1 (O) One may be inoperative provided that the GPWS or the

TAWS aural and visual warnings are checked operative.



Check of the GPWS (or TAWS) aural and visual warnings:

- PULL UP . GPWS pb-sw (operative · · · · · · · · · · Press

- Check that the GPWS (or the TAWS) aural and visualwarnings are operative.Refer to FCOM/DSC-34-70 GPWS.

34-50 ATC and Radio /

GPS Navigation

Systems

34-50-01 ATC

34-50-01A B 2 1 (O)(FD) One may be inoperative


- An altitude encoder must be operative for theoperative transponder,

- In the event both ATC transponders becomeinoperative enroute, the flight may continue to the nextpoint of intended landing where repairs or replacementfacilities are available. Appropriate authorization from

ATC centers concerned is necessary.

- An ATC transponder must be operative to enter RVSMairspace


30 JUN 12MEL

A320/321MEL/CDL 01.34.29

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-50 ATC and Radio / GPS

Navigation Systems

34-50-01 ATC



When both ATCs are inoperative, RVSM operations are

not permitted.

34-50-03 ADF

34-05-03A C 1 0 May be inoperative unless its use is required.

34-50-04 DME

34-50-04A 2 1 One may be inoperative provided both GPS is operative.

34-50-05 VOR


34-50-06 MARKER

34-50-06A C 1 0 (FD) May be inoperative provided approach minimums do not

required its use.

01.34.30NAVIGATION


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


34 NAVIGATION

34-50 ATC and Radio /

GPS Navigation

Systems

34-50-09 Global

Positioning

System (GPS)

34-50-09A 2 2 (FD) Both are required to be operative for flights departing the

kingdom envolving RNAV routes, and/or RNAV/GPS

approaches.

34-50-09B B 2 1 (O)(FD) One may be inoperative on RNAV routes, and/or

RNAV/GPS approaches returning to the kingdom provided

both DME systems are operative


Dispatch must confirm whether the route or part of the

route is RNAV airspace and destination airport does not

have published GPS approaches only.

34-50-09C B 2 0 (O)(FD) May be inoperative provided the flight is not dispatched

through RNAV airspace.


Dispatch must confirm whether the route or part of the

route is not RNAV airspace and destination, alternate

airport does not have published GPS approaches only.

* * *

30 JUN 12MEL

A320/321MEL/CDL 01.34.31

NAVIGATION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



01.34.32NAVIGATION

A320/321MEL/CDL

MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


35 OXYGEN


35-01-01 OXYGEN

Overhead Panel

35-01-01-01 CREW SUPPLY

pb-sw OFF light


35-01-01-02 PASSENGER

SYS ON light


35-01-01-31 MANUAL

Control of the

MASK MAN ON

pb

35-01-01-31A AUTO control

function

checkedoperative

C 1 0 (M) May be inoperative provided that the AUTO control

function is checked operative.


Refer to AMM 35-23-00-040-008

12 FEB 12MEL

A320/321MEL/CDL 01.35.01

OXYGEN



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


35 OXYGEN


35-01-01 OXYGEN

Overhead Panel

35-01-01-32 AUTO Control of

the MASK MAN

ON pb

35-01-01-32A C 1 0 (FD) May be inoperative provided that the operating altitude is

limited to FL 300.


DOOR/OXY SD page

35-07-01 Crew OXY High

Pressure

Indication on the

DOOR/OXY SD

page

35-07-01A C 1 0 (O)(M) May be inoperative provided that the oxygen pressure is

checked by direct reading before each flight.




Check that the oxygen pressure is sufficient for the

intended flight. Refer to FCOM/LIM-35 Cockpit Fixed

Oxygen System


Refer to AMM 35-10-00-040-001

01.35.02OXYGEN


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


35 OXYGEN


DOOR/OXY SD

page

35-07-02 Crew Oxygen

REGUL LO PR

Indication on the

DOOR/OXY SD

page

35-07-02A C 1 0 (O)(M) May be inoperative provided that the oxygen pressure is

checked before the first flight of each day.


GENERAL INFORMATION

On the DOOR/OXY SD page, disregard the REGUL LO

PR indication and the associated OXY indication.


Refer to AMM 35-10-00-040-002

35-10 Crew Oxygen


Mask

35-10-01A C 4 2 (FD) Each occupant of the cockpit must have his assigned

mask operative.


Mask Microphone

35-10-02A C 4 2 (FD) One must be operative for each pilot.

35-10-03 Exterior Crew

Oxygen

Overpressure

Indicator Disc

(Green Disc)

35-10-03A C 1 0 (O) May be missing or damaged.


12 FEB 12MEL

A320/321MEL/CDL 01.35.03

OXYGEN



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


35 OXYGEN

35-10 Crew Oxygen

35-10-03 Exterior Crew

Oxygen

Overpressure

Indicator Disc

(Green Disc)



Before the first flight of each day, check that the oxygen

pressure does not decrease:

On the DOOR/OXY SD page, check the OXY pressure

indication twice.

A 15 min interval must be applied between both checks.

35-20 Passenger Oxygen

35-20-01 Passenger

Oxygen Unit


seats

considered

inoperative

(A320)

(A321)

C

C

46

60

0

0

(FD) One or more may be inoperative provided that the

associated seats are considered inoperative.

Refer to Item 25-20-01 Passenger Seat

01.35.04OXYGEN


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


35 OXYGEN

35-20 Passenger

Oxygen


Oxygen Unit

35-20-02A (A320)

(A321)

C

C

5

7

4

5

(FD) May be inoperative provided that the associated seats are


Refer to Item 25-20-03 Cabin Attendant Seat

35-20-04 Galley Oxygen

Unit

Note:

For an inoperative cabin attendant

oxygen unit located within the galley

area: Refer to Item 35-20-02 Cabin

Attendant Oxygen Unit

35-20-04A Adjacent cabin

attendant

oxygen unit

available

B 2 0 (O) One or more may be inoperative and the associated

galley area may be occupied provided that an adjacent

cabin attendant individual oxygen unit is available for each

occupants of the associated galley area.


IN FLIGHT

The number of galley area occupants must be in

accordance with the available adjacent cabin attendant

oxygen units.

35-20-04B Portable

oxygen

available in the

associated

galley area

B 2 0 (O) One or more may be inoperative and the associated

galley area may be occupied provided that a cabin

attendant portable oxygen device is available for each

occupants of the associated galley area.


12 FEB 12MEL

A320/321MEL/CDL 01.35.05

OXYGEN



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


35 OXYGEN

35-20 Passenger Oxygen

35-20-04 Galley Oxygen

Unit



Before the flight, the flight crew shall brief the cabin crew

that the galley oxygen unit is inoperative and that thecabin attendant portable oxygen device should be used

instead.

35-20-04C Associated

galley area not

occupied

B 2 0 (FD) One o r more m ay b e inoperative p rovided t hat t he

associated galley area is not occupied.

35-20-05 Manual Release

Tool

35-20-05A C 6 1 One must be available.

35-30 Portable Oxygen

35-30-01 Flight Crew

Portable Device

35-30-01A 2 2 Both must be available.

01.35.06OXYGEN


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


35 OXYGEN

35-30 Portable Oxygen


Portable Device

35-30-02A PBE or Smoke

Hood

C 3 2 One required in the cockpit, and

One required in the cabin.

NOTE:

Any in excess of that required may beinoperative or missing provided the

inoperative PBE is placarded

inoperative, removed from the installed

location and placed out of sight so it can

not be mistaken for a functional unit.

35-30-02B Portable

Oxygen

Cylinder

May be inoperative or missing provided the inoperative

Portable Oxygen Cylinderis placarded inoperative,

removed from the installed location and placed out of

sight so it can not be mistaken for a functional unit.

(A320) C 7 4

(A321) C 8 5

* * *

12 FEB 12MEL

A320/321MEL/CDL 01.35.07

OXYGEN



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



01.35.08OXYGEN


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC

36-00 MAINTENANCE

Message on the

STATUS SD Page

36-00-01 AIR BLEED

MAINTENANCE

Message

36-00-01F C 1 - AIR BLEED MAINTENANCE message may be displayed


36-01 AIR COND

Overhead Panel

36-01-01 ENG BLEED pb-

sw FAULT light


36-01-02 ENG BLEED pb-

sw OFF light


36-01-03 APU BLEED pb-sw

FAULT light


36-01-04 APU BLEED pb-swON light


12 FEB 12MEL

A320/321MEL/CDL 01.36.01

PNEUMATIC



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC


BLEED SD page

36-07-01 APU Bleed Valve

Indication on the

BLEED SD page


36-07-02 Engine Bleed

Valve Indication

on the BLEED SD

page


36-07-03 Engine Bleed HP

Valve Indication

on the BLEED SD

page



Precooler Inlet

Pressure

Indication on the

BLEED SD page



Precooler Outlet

Temperature

Indication on the

BLEED SD page


01.36.02PNEUMATIC


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC


BLEED SD page

36-07-06 X Bleed Valve

Indication on the

BLEED SD page


36-11 Engine Bleed Air

Supply System

36-11-01 Engine Bleed Air

Supply System

Note:

The HP ground connection is near the

engine 1 hazardous area. If the bleed air

supply system 2 is inoperative, it is

better to use the APU bleed for engine

start. If the APU bleed is not available, a

ground cart can be used as long as the

pneumatic pipe is kept out of the

hazardous area.

36-11-01A no FL limitation C 2 1 (O)(FD) One may be inoperative provided that:

1) The associated ENG BLEED pb-sw is set to OFF,

2) The X-BLEED selector is set to OPEN,

3) The speedbrakes are operative, and

4) The aircraft is not operated in known or forecast icing

condations.


AFTER ENGINE START

- Refer to FCOM/PRO-ABN-36-C. AIR ENG 1(2) BLEED

FAULT and Refer to FCOM/PRO-ABN-36-B. AIR ENG

1(2) BLEED ABNORM PR.


01 MAY 12MEL

A320/321MEL/CDL 01.36.03

PNEUMATIC



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC


Supply System


Supply System


FOR TAKEOFF

Consider selecting the air conditioning packs OFF or the

APU bleed air supply system ON.

AFTER TAKEOFF

If the APU has been used to supply the air conditioning

during the takeoff, set the APU BLEED pb-sw to OFF.

IN FLIGHT

· If Wing Anti-Ice is required:

PACK (affected side) pb-sw . . . . . . . . . . . . . . . . . OFF

· In the case of failure of the remaining engine bleed

air supply system, or in the case of failure of the

associated engine:

- Apply the associated ECAM procedure, then

- Refer to QRH/ABN-36 AIR DUAL BLEED FAULT



SEQUENCE


I T E MI T E M



SEQUENCE


01.36.04PNEUMATIC


MEL

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC


Valve (PRV)


1) The affected engine bleed valve is secured in theclosed position, and

2) The associated bleed air supply system is consideredinoperative.

Refer to Item 36-11-01 Engine Bleed Air Supply System


Refer to AMM 36-11-00-040-001


Overpressure

Valve


bleed

considered

inoperative

C 2 1 One may be inoperative provided that the associated

bleed air supply system is considered inoperative.


01 MAY 12MEL

A320/321MEL/CDL 01.36.05

PNEUMATIC



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC


Supply System

36-11-04 Engine Bleed Fan

Air Valve

36-11-04A C 2 1 (FD) One may be inoperative provided that the associated

engine bleed air supply system is considered inoperative.



Precooler




36-11-06 Engine Bleed IP

Check Valve


bleed

considered

inoperative

C 2 1 (FD) One may be inoperative provided that the associated



36-11-06B Associated HP

valve secured

in the closed

position

C 2 1 (O)(M) One may be inoperative in the open position provided that

the associated HP valve is secured in the closed position.


01.36.06PNEUMATIC


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC


Supply System

36-11-06 Engine Bleed IP

Check Valve


DURING TAXI

When the engines operate in idle thrust:

- ENG (affected side) BLEED pb-sw . . . . . . . . . . . OFF

- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . OPEN

· If wing anti-ice is required:

One PACK pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF

DURING TAKEOFF, CLIMB, AND CRUISE

- ENG (affected side) BLEED pb-sw . . . . . . . . . . . On

- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . AUTO

DURING DESCENT

When the engines operate in idle thrust:

- ENG (affected side) BLEED pb-sw . . . . . . . . . . . OFF


· If wing anti-ice is required:

One PACK pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF


Refer to AMM 36-11-00-040-002

12 FEB 12MEL

A320/321MEL/CDL 01.36.07

PNEUMATIC



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC


Supply System

36-11-07 Engine Bleed HP

Valve


bleed

considered

inoperative

C 2 1 (FD) One may be inoperative in the closed position provided

that the associated engine bleed air supply system is



36-11-07B HP valve

secured in the

closed position

C 2 1 (O)(M) One may be inoperative provided that the affected engine

bleed HP valve is secured in the closed position.


Refer to MEL item 36-11-06B


Refer to AMM 36-11-00-040-003

36-11-08 Bleed Monitoring

Computer (BMC)

36-11-08A C 2 1 (FD) One may be inoperative provided that the associated



01.36.08PNEUMATIC


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC

36-12 APU Bleed Air

Supply and

Crossbleed

Systems

36-12-01 APU Bleed Air

Supply System

36-12-01A C 1 0 May be inoperative provided that the APU BLEED pb-sw

is set to OFF.

36-12-02 APU Bleed Valve

36-12-02A APU bleed

considered

inoperative

C 1 0 (M) May be inoperative provided that:

1) The APU bleed valve is secured in the closed position,and

2) The APU bleed air supply system is consideredinoperative.

Refer to Item 36-12-01 APU Bleed Air Supply System


Refer to AMM 36-12-00-710-001

36-12-02B APU not used C 1 0 (O) May be inoperative in the open position provided that the

APU is not used in flight.

Refer to Item 49-10-01 Power Plant (APU)



· When the APU runs:

APU BLEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . ON

· After APU shutdown:

APU BLEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . Off

12 FEB 12MEL

A320/321MEL/CDL 01.36.09

PNEUMATIC



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC

36-12 APU Bleed Air Supply

and Crossbleed

Systems

36-12-03 APU Bleed Check

Valve

36-12-03A C 1 0 May be inoperative provided that the APU bleed air supply


Refer to Item 36-12-01 APU Bleed Air Supply System

36-12-04 Automatic Control

of the X Bleed

Valve

36-12-04A C 1 0 (O) May be inoperative provided that the manual control is

checked operative.



Check of the manual control of the X BLEED valve:


- On the BLEED, check that the cross bleed valve is

indicated open.

- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . SHUT

- On the BLEED, check that the cross bleed valve is

indicated closed.

- X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . AUTO

01.36.10PNEUMATIC


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


36 PNEUMATIC

36-22 Leak Detection

Loop

36-22-01 Pylon Leak

Detection System


1) The associated pylon leak detection loop isdeactivated, and

2) The AIR ENG 1(2) BLEED LEAK alert is confirmed tobe false by troubleshooting, and

3) The associated bleed air supply system is consideredinoperative.



Refer to AMM 36-22-00-040-001

36-22-02 Wing Leak

Detection System


Note:

Failure of one loop in one or both wing

leading edges is indicated by a

MAINTENANCE message displayed on

the STATUS SD page.

Refer to Item 36-00-01 AIR BLEED MAINTENANCE

Message

36-22-03 APU LeakDetection Loop


* * *

12 FEB 12MEL

A320/321MEL/CDL 01.36.11

PNEUMATIC



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



01.36.12PNEUMATIC


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


38 WATER/WASTE

-10-01 Potable Water Systems C 1 0 (M) Individual components may be inoperative provided:a) Associated components are deactivated or isolated,

andb) Associated system components are verified not to

have leaks.

NOTE:

Any portion of system which is operative

may be used.


Refer to AMM 38-10-00

C 1 0 (M) May be inoperative provided:a) System is drained, andb) Procedures are established to ensure that system is

not serviced.



-30-01 Lavatory Waste

Systems (Including

Wheelchair Accessible

Lavatories)

C 1 0 (M) Individual components may be inoperative provided:a) Associated components are deactivated or

isolated,andb) Associated system components are verified not to

have leaks.

NOTE:

Any portion of system which is operative

may be used.




12 FEB 12

MEL

A320/321MEL/CDL 01.38.01

WATER/WASTE

I T E M



SEQUENCE


7/23/2019 A 320321 Mel Cdl


38 WATER/WASTE

-30-01 Lavatory Waste

Systems (Including

Wheelchair Accessible

Lavatories)

(Cont’d)

C 1 0 (M)(FD) Associated Lavatory system(s) may be inoperative

provided:a) Associated components are deactivated or isolated to

pervent leaks,b) Extra safety pilot should be assigned to operate the

flight in case the forward lavatory placarded,c) Associated Lavatory door (s) is secured closed and

placarded, “INOPERATIVE - DO NOT ENTER”, andd) Two lavatories must be operative.

NOTE:

These provisions are not intended to

prohibit inspections by crew members.



1) Vacuum Generator

Systems (Toilet)

C 2 0 (M)(FD) May be inoperative provided:a) Vacuum generator is deactivated, and

b) Procedures are established and used toonly allow use of the associated lavatory

at or above 16000 FT MSL.



* * *

01.38.02

WATER/WASTE

A320/321MEL/CDL 04 APR 12

MEL

I T E M



SEQUENCE


7/23/2019 A 320321 Mel Cdl


46 INFORMATION SYSTEM

46-11 Aircraft

Information

Network Systems

46-11-01 Electronic Flight

Bag (EFB)

46-11-01A B 2 0 (FD) One or both may be inoperative provided that the

following documents must be provided to the FDC by

dispatch:

1. Flight Dispatch Release and attachments.(including ATS FP)

2. Computer Flight Plan or manual flight log.

3. NOTAMS.

4. Latest current available TAFs/ METARs.

5. Temporary/ MTTL takeoff and landing preformancecharts (when applicable) and takeoff data cards.

6. NOTOC (if applicable).

7. ASR/ Flight Crew Report forms.

8. Manual Loadsheet Calculation Form.

46-21 Air Traffic and

Information

Management

System

46-21-01 Air Traffic Service

Unit (ATSU)

46-21-01A B 1 0 (O)(FD) May be inoperative provided altenate procedures are

used.


12 FEB 12MEL

A320/321MEL/CDL 01.46.01

INFORMATION SYSTEM



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


46 INFORMATION SYSTEM

46-21 Air Traffic and

Information

Management System

46-21-01 Air Traffic Service

Unit (ATSU)


1) Flight crew must transmit depature, enroute, and the

arrival reports in accordance with the route manualcommunication requirement.

2) Flight crew must complete the in-flight cruiseperformance data records if required.

Note:

Any portion of the system that is

operative may be used

46-21-02 Datalink Control

and Display Unit

(DCDU)

46-21-02A B 2 0 (FD) One or both may be inoperative provided two way

communications established with ATC and inroute not

require its use.

46-21-03 ATC MSG pb

46-21-03A B 2 0 (FD) Refer to MEL 46-21-02A

* * *

01.46.02INFORMATION SYSTEM


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


47 INERT GAS SYSTEM

47-00 MAINTENANCE

Message on the

STATUS SD Page

47-00-01 FUEL INERT

MAINTENANCE

Message

47-00-01A C 1 - FUEL INERT MAINTENANCE Message may be displayed


* * *



SEQUENCE


I T E MI T E M



SEQUENCE


12 FEB 12MEL

A320/321MEL/CDL 01.47.01

INERT GAS SYSTEM

7/23/2019 A 320321 Mel Cdl



01.47.02INERT GAS SYSTEM


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


49 AIRBORNE AUXILIARY

POWER

49-00 MAINTENANCE

Message on the

STATUS SD page

49-00-01 APU

MAINTENANCE

Message

49-00-01A C 1 - APU MAINTENANCE message may be displayed on the

STATUS SD page.

49-01 APU Overhead

Panel

49-01-01 APU MASTER SW

pb-sw FAULT light

49-01-01A C 1 0 May be inoperative provided that the N and the EGT

indications are operative on the APU SD page.

49-01-02 APU MASTER SW

pb-sw ON light

49-01-02 C 1 0 May be inoperative.

49-01-03 APU START pb-sw

AVAIL light

49-01-03A C 1 0 May be inoperative provided that the N indication is

operative on the APU SD page.

49-01-04 APU START pb-sw

ON light


12 FEB 12MEL

A320/321MEL/CDL

01.49.01 AIRBORNE AUXILIARY

POWER



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


49 AIRBORNE AUXILIARY

POWER


APU SD page


APU SD page


49-10 Power Plant

49-10-01 Power Plant (APU)



GENERAL INFORMATION

No APU bleed air will be available for Main Engine Start

(MES) or air conditioning.

No electrical power will be available from the APU

generator.


APU MASTER SW pb-sw . . . . . . . . . . . . . . . . . . . Off

49-10-02 APU Air Intake

Flap

49-10-02A APU not used C 1 0 May be inoperative in the closed position provided that the

APU is not used.

49-10-02B APU used A 1 0 (M) May be inoperative in the open position for 10 days.


Refer to AMM 49-16-00-040-002

* * *

01.49.02 AIRBORNE AUXILIARYPOWER


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


52-01-01 CKPT DOOR

CONT Normal

Overhead Panel

52-01-01-01 CHAN (1, 2)

LEDs on the

CKPT DOOR

CONT Overhead

Panel


52-01-01-02 STRIKE (TOP,

MID, BOT) LEDs

on the CKPT

DOOR CONT

Overhead Panel


52-01-01-03 Pressure RateSensor on the

CKPT DOOR

CONT Overhead

Panel

52-01-01-03A One inoperative A 2 1 (M) One may be inoperative for 60 consecutive calendar

days provided that the remaining pressure rate sensor is

checked operative.


Refer to AMM 52-51-00-040-011

52-01-01-03B Both

inoperative

C 2 0 Both may be inoperative provided that the CDLS normal


Refer to Item 52-51-01 CDLS Normal System (Normal

Control Unit, Switch and Lights on the CKPT DOOR

Panel, Buzzer, Keypad).

12 FEB 12MEL

A320/321MEL/CDL 01.52.01

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


52-01-02 CKPT DOOR

CONT BK UP

Overhead Panel

52-01-02-01 CHAN (1, 2)

LEDs on the

CKPT DOOR

CONT BK UP

Overhead Panel

52-01-02-01A CTL pb FAULT

light checked

operative

C 2 0 (O) One or more may be inoperative provided that the CTL pb

FAULT light is checked operative.




- Check that the associated CTL pb FAULT light comes

on.

52-01-02-01B CDLS back-up

system

considered

inoperative

C 2 0 One or more may be inoperative provided that the CDLS

back-up system is considered inoperative.

Refer to Item 52-51-02 CDLS BK UP System (Back-up

Control Unit, CTL pb and Lights on the CKPT DOOR BK

UP Panel)

01.52.02DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


52-01-02 CKPT DOOR

CONT BK UP

Overhead Panel

52-01-02-02 STRIKE (TOP,

MID, BOT) LEDs

on the CKPT

DOOR CONT BK

UP Overhead

Panel

52-01-02-02A CTL pb FAULT

light checked

operative

C 3 2 (O) One may be inoperative provided that the CTL pb FAULT

light is checked operative.




- Check that the associated CTL pb FAULT light comeson.

52-01-02-02B CDLS back-up

system

considered

inoperative

C 3 0 One or more may be inoperative provided that the CDLS

back-up system is considered inoperative.



UP Panel)

12 FEB 12MEL

A320/321MEL/CDL 01.52.03

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


52-01-02 CKPT DOOR

CONT BK UP

Overhead Panel

52-01-02-03Pressure Rate

Sensor on the

CKPT DOOR

CONT BK UP

Overhead Panel

52-01-02-03A One

inoperative

A 2 1 (M) One may be inoperative for 60 consecutive calendar

days provided that the remaining pressure rate sensor is

checked operative.


Refer to AMM 52-51-00-040-012

52-01-02-03B Both

inoperative

C 2 0 Both may be inoperative provided that the CDLS back-up




UP Panel)

01.52.04DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


52-01-03 CKPT DOOR BK

UP Overhead

Panel

52-01-03-01 CTL pb FAULT

light on the

CKPT DOOR BK

UP Overhead

Panel




· To ensure that the door is closed and locked:

On the CKPT DOOR CONT BK UP panel, check that the

three STRIKE LEDs are off.

52-01-03-01B C 1 0 May be inoperative provided that the CDLS back-up




UP Panel)

12 FEB 12MEL

A320/321MEL/CDL 01.52.05

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-01 Overhead Panel


UP Overhead

Panel

52-01-03-02 CTL pb OPEN

light on the

CKPT DOOR BK

UP Overhead

Panel




· To ensure that the door is closed and locked:

On the CKPT DOOR CONT BK UP panel, check that the

three STRIKE LEDs are off.





UP Panel)

01.52.06DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS



UP Overhead

Panel

52-01-03-31 CTL pb on the

CKPT DOOR BK

UP Overhead

Panel



- Manual opening from the cockpit has to be performed by

the cockpit crew.

One additional crew member must lock or unlock the

cockpit door manually whenever access to the flight deck

is granted or one of the crew leaves the cockpit.





UP Panel)

12 FEB 12MEL

A320/321MEL/CDL 01.52.07

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS



UP Overhead

Panel

52-01-03-32 BK UP Function

of the LKG SYS

sw on the CKPT

DOOR BK UP

Overhead Panel

52-01-03-32A C 1 0 May be inoperative provided that the CDLS back-up




UP Panel)

52-01-03-33 NORM Function

of the LKG SYS

sw on the CKPT

DOOR BK UP

Overhead Panel

52-01-03-33A C 1 0 May be inoperative provided that the CDLS normal


Refer to Item 52-51-01 CDLS Normal System (Normal

Control Unit, Switch and Lights on the CKPT DOOR

Panel, Buzzer, Keypad)

01.52.08DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS



UP Overhead

Panel (cont’d)

52-01-03-34 OFF Function of

the LKG SYS sw

on the CKPT

DOOR BK UP

Overhead Panel

52-01-03-34A C 1 0 (M) May be inoperative.

Note:

For maintenance purpose only, the

CDLS normal and the CDLS back-up

systems can be deactivated by

performing the associated maintenance

procedure.


Refer to AMM 52-51-00-040-008

12 FEB 12MEL

A320/321MEL/CDL 01.52.09

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page


Permanently

Indicated Open on

the DOOR/OXY SD

page

(A320)

52-07-01A Check of

associated door

and 'C' repair

interval

C 4 0 (O)(FD) One or more may be permanently indicated open when

actually closed provided that:

1) The associated door is visually checked to be closedand locked before each flight, and

2) The white SLIDE ARMED light on the associateddoor does not come on when the door is closed andlocked and the slide arming lever is in the armedposition.


GENERAL INFORMATION

If passenger doors are affected, indications on the PTP or

the FAP may be affected.

If passenger doors are affected, the time recorded in the

ACARS movement report may be wrong.

AFTER ENGINE START

· In the case of false door alert:

EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press

Note:the limitation MAX FL : 100/MEA

remains displayed on the STATUS SD

page.


01.52.10DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD

page


Permanently

Indicated Open on

the DOOR/OXY SD

page

(A320)

52-07-01A Check of

associated door

and 'C' repair

interval (cont’d)


BEFORE TAKEOFF

- T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press

In the T.O MEMO, the "T.O CONFIG NORMAL" line will

not replace the "T.O CONFIG . . TEST" line.

- Consider normal configuration for takeoff provided that

no alert was displayed during the T.O CONFIG TEST.

CAUTION

The T.O CONFIG pb must be


is no alert.

12 FEB 12MEL

A320/321MEL/CDL 01.52.11

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page


Permanently

Indicated Open on

the DOOR/OXY SD

page

(A320)

52-07-01B Check of

associated door

and 'B' repair

interval

B 4 0 (O)(FD) One or more may be permanently indicated open when

actually closed provided that the associated door is

visually checked to be closed and locked before each

flight.


GENERAL INFORMATION

If passenger doors are affected, indications on the PTP or

the FAP may be affected.



The SLIDE ARMED light on passenger doors may be

permanently illuminated.

AFTER ENGINE START



Note:

the limitation MAX FL : 100/MEA

remains displayed on the STATUS SDpage.


01.52.12DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD

page


Permanently

Indicated Open on

the DOOR/OXY SD

page

(A320)

52-07-01B Check of

associated door

and 'B' repair

interval (cont’d)


BEFORE TAKEOFF






CAUTION



is no alert.

52-07-01C No night

operations




2) The associated door is visually checked to be closed

and locked before each flight.



12 FEB 12MEL

A320/321MEL/CDL 01.52.13

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page

52-07-01 Passenger

Door/Emergency

Exit Permanently

Indicated Open on

the DOOR/OXY SD

page

(A321)

52-07-01A Check of

associated door

and 'C' repair

interval



1) The associated door is visually checked to be closedand locked before each flight, and

2) The white SLIDE ARMED light on the associateddoor does not come on when the door is closed andlocked and the slide arming lever is in the armedposition.


GENERAL INFORMATION

If passenger doors/emergency exits are affected,

indications on the PTP or the FAP may be affected.




01.52.14DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD

page

52-07-01 Passenger

Door/Emergency

Exit Permanently

Indicated Open on

the DOOR/OXY SD

page

(A321)

52-07-01A Check of

associated door

and 'C' repair

interval (cont’d)


AFTER ENGINE START



Note:


remains displayed on the STATUS SDpage.

BEFORE TAKEOFF






CAUTION



is no alert.

12 FEB 12MEL

A320/321MEL/CDL 01.52.15

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page

52-07-01 Passenger

Door/Emergency

Exit Permanently

Indicated Open on

the DOOR/OXY SD

page

(A321)

52-07-01B Check of

associated door

and 'B' repair

interval

B 8 0 (O)(FD) One or more may be permanently indicated open when

actually closed provided that the associated door is

visually checked to be closed and locked before each

flight.


GENERAL INFORMATION



If passenger doors are affected, the time recorded in the ACARS movement report may be wrong.

The SLIDE ARMED light on passenger doors/emergency

exit may be permanently illuminated.

AFTER ENGINE START



Note:

the limitation MAX FL : 100/MEAremains displayed on the STATUS SD

page.


01.52.16DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD

page

52-07-01 Passenger

Door/Emergency

Exit Permanently

Indicated Open on

the DOOR/OXY SD

page

(A321)

52-07-01B Check of

associated door

and 'B' repair

interval (cont’d)


BEFORE TAKEOFF






CAUTION



is no alert.

52-07-01C No night

operations




2) The associated door is visually checked to be closed

and locked before each flight.



12 FEB 12MEL

A320/321MEL/CDL 01.52.17

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page


Permanently

Indicated Closed

on the DOOR/OXY

SD page

(A320)

52-07-02A No night

operations

C 4 0 (O)(FD) One or more may be permanently indicated closed when

actually open provided that:


2) The associated door is visually checked to be closedand locked before each flight.


GENERAL INFORMATION

If passenger doors are affected, indications on the PTP or the FAP may be affected.



01.52.18DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD

page

52-07-02 Passenger

Door/Emergency

Exit Permanently

Indicated Closed

on the DOOR/OXY

SD page

(A321)

52-07-02A No night

operations

C 8 0 (O)(FD) One or more may be permanently indicated closed when



2) The associated door is visually checked to be closedand locked before each flight.


GENERAL INFORMATION





12 FEB 12MEL

A320/321MEL/CDL 01.52.19

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page

52-07-03 Overwing

Emergency Exit

Permanently

Indicated Open on

the DOOR/OXY SD

page

52-07-03A Check of

associated exit

and 'C' repair

interval

C 2 0 (O)(M)

(FD)

One or both may be permanently indicated open when


1) The associated exit is visually checked to be closedand locked before each flight, and

2) The relevant SLIDE indication on the DOOR/OXYSD page is normally displayed in white.


GENERAL INFORMATION

Indications on the PTP or the FAP ñ– may be affected.

AFTER ENGINE START



Note:



page.


01.52.20DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD

page

52-07-03 Overwing

Emergency Exit

Permanently

Indicated Open on

the DOOR/OXY SD

page

52-07-03A Check of

associated exit

and 'C' repair

interval (cont’d)


BEFORE TAKEOFF





no alert were displayed during the T.O CONFIG TEST.

CAUTION



is no alert.


Refer to AMM 52-70-00-040-010

12 FEB 12MEL

A320/321MEL/CDL 01.52.21

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page

52-07-03 Overwing

Emergency Exit

Permanently

Indicated Open on

the DOOR/OXY SD

page (A320)

52-07-03B Check of

associated exit

and 'B' repair

interval

B 2 0 (O)(M) One or both may be permanently indicated open when

actually closed provided that the associated exit is visually

checked to be closed and locked before each flight.




Refer to AMM 52-70-00-040-010

52-07-03C No night

operations

C 2 0 (O)(M)

(FD)

One or more may be permanently indicated open when



2) The associated exit is visually checked to be closedand locked before each flight.




Refer to AMM 52-70-00-040-010

01.52.22DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD

page

52-07-04 Overwing

Emergency Exit

Permanently

Indicated Closed

on the DOOR/OXY

SD page (A320)

52-07-04A No night

operations

C 2 0 (O)(M)

(FD)

One or more may be permanently indicated closed when



2) The associated exit is visually checked to be closedand locked before each flight.


GENERAL INFORMATION

Indications on the PTP or the FAP may be affected.


Refer to AMM 52-70-00-040-011

12 FEB 12MEL

A320/321MEL/CDL 01.52.23

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page

52-07-05 Cargo Door

Indication on the

DOOR/OXY SD

page

52-07-05A C 3 0 (O)(M)

(FD)

One or more may be inoperative provided that the

associated door is visually checked to be closed and

locked before each flight.


GENERAL INFORMATION

· If cargo indication is inoperative due to a proximity

switch failure:

The relevant cargo heating is inhibited. Live animals must

not be carried in the cargo.

AFTER ENGINE START



Note:



page.


01.52.24DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD

page

52-07-05 Cargo Door

Indication on the

DOOR/OXY SD

page


BEFORE TAKEOFF






CAUTION


maintained pressed to check that thereis no alert.


Refer to AMM 52-70-00-040-001

52-07-06 Avionics

Compartment

Access Door

Indication on the

DOOR/OXY SD

page

52-07-06A C 4 0 (O)(M)

(FD)

One or more may be inoperative provided that the

associated door is visually checked to be closed and

locked before each flight.


12 FEB 12MEL

A320/321MEL/CDL 01.52.25

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


DOOR/OXY SD page

52-07-06 Avionics

Compartment

Access Door

Indication on the

DOOR/OXY SD

page


AFTER ENGINE START



Note:



page.

BEFORE TAKEOFF





no alert were displayed during the T.O CONFIG TEST.


Refer to AMM 52-70-00-040-004

01.52.26DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-10 Passenger/Crew

Door

52-10-01 Cabin Passenger

Door


52-10-02 Overwing

Emergency Exit

(A320)


52-10-03 Passenger Exit

Stop Fitting

52-10-03A (A320)

(A321)

C

C

56

96

52

90

(FD) A maximum of one per exit may be inoperative provided

that the flight is not pressurized, and


Pressurized.

Flight must be conducted in accordance with FOPM CH 8


52-10-04 Door Damper

Function

(A320)


52-10-04 Door Damper

Function

(A321)


12 FEB 12MEL

A320/321MEL/CDL 01.52.27

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-10 Passenger/Crew Door

52-10-05 Door Emergency

Opening Function

52-10-05A (A320)

(A321)

4

8

4

8

52-10-06 CHECK DOOR

PRESSURE

Message on the

Flight Attendant

Panel (FAP)

52-10-06A (A320)

(A321)

C

C

4

8

0

0

(M) One or more messages may be displayed provided that

the door bottle pressure is checked on the associated

bottle pressure gauge before the first dispatch and then

every 8 days.


Refer to AMM 52-00-00-040-003


Stay Mechanism

52-10-07A (A320)

(A321)

4

8

4

8

01.52.28DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-10 Passenger/Crew

Door

52-10-08 CABIN PRESSURE

light (on Doors)

52-10-08A (A320)

(A321)

C

C

4

8

0

0

One or more may be inoperative.

52-30 Cargo Door

52-30-01 Cargo Door (FWD,

AFT and BULK)

52-30-01A Cargo door

indicated locked

on the

DOOR/OXY SD

page

C 3 0 One or more may be inoperative in the closed and locked

position provided that they are indicated locked on the

DOOR/OXY SD page.

52-30-01B Visual check of

the cargo door

C 3 0 (M) One or more may be inoperative in the closed and locked

position provided that the associated cargo door isvisually checked to be closed and locked before each

flight.


Refer to AMM 52-30-00-040-001

52-30-02 Cargo Door

Actuator

52-30-02A A maximum of

one actuator

inoperative per

cargo door

A 4 2 (FD) A maximum of one per cargo door may be inoperative

provided that:

1) The integrity of the yellow hydraulic system is notaffected, and

2) The wind velocity during loading and unloadingoperations is below 30 kt, and

3) The operation of the door with a single actuator islimited to 100 open/close cycles.

12 FEB 12MEL

A320/321MEL/CDL 01.52.29

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-30 Cargo Door

52-30-02 Cargo Door

Actuator


actuator

inoperative


1) The integrity of the yellow hydraulic system is notaffected, and

2) The associated cargo door is manually closed and

locked.


Refer to AMM 52-36-00-040-001

52-30-03 Cargo Door

Electrical Control

52-30-03A Cargo door

operated using

hand pump


associated cargo doors can be operated using the hand

pump.

52-30-03B Cargo door considered

inoperative

C 2 0 (FD) One o r more m ay b e inoperative p rovided t hat t heassociated cargo doors are considered inoperative.

Refer to Item 52-30-01 Cargo Door (FWD, AFT)

52-30-04 Cargo Door

Locking Hooks

and Spools

(Rollers)

52-30-04A (Hooks)

(Spools)

C

C

14

14

11

11

(FD) A maximum of one locking hook or one spool per cargo

door may be inoperative provided that:

1) All the others have no damage, and



Pressurized.



01.52.30DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-30 Cargo Door

52-30-05 Cargo Door Hand

Pump

52-30-05A C 1 0 May be inoperative provided that the integrity of the yellow

hydraulic system is not affected.

52-30-06 Cargo Door Drift

Pin

52-30-06A A 4 0 One or both on each cargo door may be inoperative for

one flight.

52-30-07 Cargo Doors

Open/Locked

Indicator light

52-30-07A C 2 0 (O) One or both may be inoperative provided that the

associated cargo door is in the fully open position during

loading and unloading operations.


ON GROUND

· When the Cargo Door Open/Locked Indicator light

is inoperative, it is necessary to inform the ground

personnel:

- To visually check that the affected cargo door is in the

fully open position, with no downward movement after

releasing the lever of the manual selector valve.

- To visually check that the lever of the manual selector

valve stays in the neutral position.

12 FEB 12MEL

A320/321MEL/CDL 01.52.31

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-33 Bulk Cargo

Compartment Door

52-33-01 Cargo Door

Balance

Mechanism

52-33-01A C 1 0 (M) May be inoperative or damaged provided that:

1) A safety hold device is used to maintain the cargo

door in the open position during loading andunloading operations, and

2) The associated cargo door is visually checked to beclosed and locked.


Refer to AMM 52-33-00-040-001

52-51 Reinforced Cockpit

Door (CDLS)

52-51-01 CDLS Normal

System (NormalControl Unit,

Switch and Lights

on the CKPT

DOOR Panel,

Buzzer, Keypad)

Note:

Any part of the CDLS may beinoperative provided the complete

system is deactivated in the unlocked

position and is not required by

operational regulations for the intended

flight.

52-51-01A CDLS back-up

control unit

operative


1) The interphone system between the cabin and thecockpit is operative, and

2) The LKG SYS selector on the CKPT DOOR BK UPpanel is set to the BK UP position , and

3) The CDLS back-up control unit is operative.


01.52.32DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-51 Reinforced

Cockpit Door

(CDLS)

52-51-01 CDLS Normal

System (Normal

Control Unit,

Switch and Lights

on the CKPT

DOOR Panel,

Buzzer, Keypad)

52-51-01A CDLS back-up

control unit

operative

(cont’d)


PIC brief cabin crew before departure to use the cabin

interphone to communicate with the cockpit crew to

request access to the cockpit, and

A third crew member must be available in the cockpit

when a flight crew member leaves the cockpit during flight


LKG SYS sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BK UP

The CDLS keypad operation is not available in back-up

mode.

The cockpit crew must brief the cabin crew that the CDLS

keypad is inoperative.

IN FLIGHT

At least two people must always be present in the cockpitthroughout the entire flight.

12 FEB 12MEL

A320/321MEL/CDL 01.52.33

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


Door (CDLS)

52-51-02 CDLS BK UP

System (Back-up

Control Unit, CTL

pb and Lights on

the CKPT DOOR

BK UP Panel)


52-51-03 CDLS Buzzer

52-51-03A C 1 0 (O) May be inoperative provided:

1) Keypad is deactivated, and

2) Alternate procedures are established and used.


Flight attendants shall be briefed not to use the keypad

and instead use interphone and pre-arranged knocks on

the door when entry is required.

52-51-04 CDLS Keypad

52-51-04A C 1 0 (O)(M)

(FD)

May be inoperative provided :

1) The interphone system between the cabin and thecockpit is operative, and

2) The keypad is deactived.


01.52.34DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-51 Reinforced

Cockpit Door

(CDLS)



1. Flight attendants shall be briefed on an alternate flightdeck entry procedure which requires the use of cabin

interphone and a specified sequence of knocks on thedoor.

2. A third crew member must be available in the cockpitwhen a flight crew member leaves the cockpit duringflight.


Refer to AMM 52-51-00-040-007


Green and RedLEDs

52-51-05A C 2 0 (O)(FD) May be inoperative provided alternate procedures are



1. Flight attendants shall be briefed on an alternate flightdeck entry procedure which requires the use of cabininterphone and a specified sequence of knocks on thedoor.

2. A third crew member must be available in the cockpitwhen a flight crew member leave the cockpit duringflight.

12 FEB 12MEL

A320/321MEL/CDL 01.52.35

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS


Door (CDLS)

52-51-06 CDLS Door

Release Strike

(Catch, Spring,

Solenoid, Bolt)

52-51-06A C 3 2 (M) One may be inoperative provided associated door release

strike is deactivated or removed.

NOTE:

Application of the maintenance

procedure is only necessary when the

inoperative door release strike is failed

in locked position.


Refer to AMM 52-51-00-040-010

52-53 COCKPIT DOOR Panel

on the Center Pedestal

52-53-01 COCKPIT DOOR

FAULT light

52-53-01 B 1 0 (M) May be inoperative provided:

1) Automatic lock controls are verified operative, and

2) Door chime is operative.


Refer to AMM 52-51-00-810-801

01.52.36DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-53 COCKPIT DOOR

Panel on the

Center Pedestal

52-53-02 COCKPIT DOOR

OPEN light

52-53-02A B 1 0 May be inoperative provided automatic lock controls are

verified operative.

52-53-03 LOCK Function of

the COCKPIT

DOOR sw

52-53-03A B 1 0 (O) May be inoperative provided:

1) The cockpit door locking system keypad isdeactivated.

2) Alternate procedures are established and used.



52-53-04 UNLOCK Function

of the COCKPIT

DOOR sw

52-53-04A B 1 0 (O) May be inoperative provided alternate procedures are



One additional crew member must lock or unlock the

cockpit door manually whenever access to the flight deckis granted or one of the crew leaves the cockpit.

* * *

01 MAY 12MEL

A320/321MEL/CDL 01.52.37

DOORS



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



01.52.38DOORS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


56 WINDOWS

56-10 Cockpit

56-10-01 Front Windshield Note:

A cockpit window with minor damages

(as described in the associated

maintenance procedure) is considered

operative, but the vision through this

cockpit window must be acceptable to

the flight crew.

56-10-01C For SPS

Windshields

(P/N STA320-1-

3-1 and

STA320-2-3-1)

A 2 2 (O)(M)

(FD)

One front windshield external ply may be cracked for one

flight provided that:

1) The other front windshield is not damaged, and

2) The associated windshield heating is deactivated, and

3) The visibility through the associated front windshield isacceptable to the flight crew, and

4) The aircraft is not operated in known or forecast icingconditions.



< When PF side is affected:


< When PNF side is affected:

Maximum landing capability is not affected and is still

CAT II.


Refer to AMM 56-10-00-040-001

12 FEB 12MEL

A320/321MEL/CDL 01.56.01

WINDOWS



SEQUENCE


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7/23/2019 A 320321 Mel Cdl


56 WINDOWS

56-10 Cockpit

56-10-01 Front Windshield

56-10-01D For SPS

Windshields

(only P/N

STA320-1-3-1

and STA320-2-

3-1)

C 2 2 (O)(M)

(FD)

One front windshield may have burn spots in the bus bar

area beyond the limits provided that:

1) The other front windshield is not damaged, and

2) The associated windshield heating is deactivated,and

3) The visibility through the associated front windshieldis acceptable to the flight crew, and

4) The aircraft is not operated in known or forecasticing conditions.



< When PF side is affected:


< When PNF side is affected:

Maximum landing capability is not affected and is still

CAT II.


Refer to AMM 56-10-00-040-001

56-10-02 Lateral

Fixed/Sliding

Window

Note:

A cockpit window with minor damages

(as described in the associated

maintenance procedure) is consideredoperative, but the vision through this

cockpit window must be acceptable to

the flight crew.

01.56.02WINDOWS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


56 WINDOWS

56-10 Cockpit

56-10-03 Sliding Window

Opening/Closing

Mechanism


56-20 Cabin

56-20-01 Cabin Window

56-20-01A (A320)

(A321)

A

A

36

44

30

40

(FD) One or more may be cracked for one flight day provided

that the flight is not pressurized.


Pressurized.


Maintenance Ferry Flight

* * *

12 FEB 12MEL

A320/321MEL/CDL 01.56.03

WINDOWS



SEQUENCE


I T E M

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01.56.04WINDOWS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


70 ENGINE

70-00 MAINTENANCE

Messages on the

STATUS SD page

70-00-01 ENG FADEC

MAINTENANCE

Message

70-00-01B For Engines

Affected by

CFM VSB 73-

0241

A 1 - ENG FADEC MAINTENANCE message may be displayed

on the STATUS SD page for 25 flight hours or 3 days,

whichever occurs first.

70-00-01C For Engines

Affected by

CFM VSB 73-

0241

C 1 - (M) ENG FADEC MAINTENANCE message may be displayed

on the STATUS SD page provided it is checked before

the first flight of each day that the CFDS does not report

any fault on a T12 sensor.


Refer to AMM 73-29-00-040-001

70-00-02 ENG EIU

MAINTENANCEMessage

70-00-02A C 1 - ENG EIU MAINTENANCE message may be displayed on

the STATUS SD page.

70-00-03 ENG EVMU

MAINTENANCE

Message

70-00-03A C 1 - ENG EVMU MAINTENANCE message may be displayed


* * *

12 FEB 12MEL

A320/321MEL/CDL 01.70.01

ENGINE



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl



01.70.02ENGINE


MEL



SEQUENCE


I T E M

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73 ENGINE FUEL

AND CONTROL


ENGINE SD page

73-07-01 F. USED Indication

on the ENGINE SD

page

73-07-01A One indication

inoperative

C 2 1 One may be inoperative provided that the fuel quantity

indications of the associated tanks are operative on the

FUEL SD page.

73-07-02 Fuel Filter Clog

Indication on the

ENGINE SD page



EWD

73-08-01 Fuel Flow

Indication on the

EWD


12 FEB 12MEL

A320/321MEL/CDL

01.73.01ENGINE FUEL

AND CONTROL



SEQUENCE


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73 ENGINE FUEL

AND CONTROL

73-09 ECAM Alert

73-09-01 ENG 1(2) FUEL

FILTER CLOG

Alert

73-09-01A C 2 1 (M) One may be displayed provided that:

1) The alert is confirmed to be false by troubleshooting,

and2) The associated filter is replaced every day.


Refer to AMM 73-30-00-040-043

73-10 Distribution

73-10-01 Fuel Return Valve


closed position

C 2 1 One may be inoperative in the closed position on one

engine provided that the APU and the AC auxiliary

generation are operative.


open position

C 2 0 One or both may be inoperative in the open position

provided that the four wing tank pumps are operative.

73-10-03 Fuel Metering

Valve


73-20 Controlling

73-20-01 Flex Takeoff

Mode

73-20-01A C 2 0 May be inoperative on one or both engines provided that

the maximum thrust is used for takeoff.

01.73.02ENGINE FUEL

AND CONTROL


MEL



SEQUENCE


I T E M

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73 ENGINE FUEL

AND CONTROL

73-20 Controlling

73-20-05 Minimum Idle on

Ground

73-20-05A C 2 0 (O) One or both may be inoperative provided that the Flight

Manual performance penalties are applied.






Flight Dispatch or use the following penalties for takeoff

and landing performance determination if MTTL charts are

not available.

Takeoff must be performed with full thrust.

VMCG/VMCA limitation No VMCG/VMCAlimitation


V1, VR, V2 decrement

(kt IAS)0 2

Landing performance:

No penalty.


30 JUN 12MEL

A320/321MEL/CDL

01.73.03ENGINE FUEL

AND CONTROL



SEQUENCE


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73 ENGINE FUEL

AND CONTROL

73-20 Controlling

73-20-05 Minimum Idle on

Ground






Flight Dispatch or use the following penalties for takeoff

and landing performance determination if MTTL charts are

not available..

Takeoff must be performed with full thrust.

VMCG/VMCA limitationNo VMCG/VMCA

limitation


V1, VR, V2 decrement

(kt IAS)0 1

Landing performance:

No penalty.

* * *

01.73.04ENGINE FUEL

AND CONTROL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


74 IGNITION


ENGINE SD page

74-07-01 Selected Igniter

Indication on the

ENGINE SD page

74-07-01A C 4 0 (O) One or more may be inoperative provided that the

associated ENG 1(2) IGN A(B)(A+B) FAULT alert is

checked operative.


AFTER ENGINE START

· If engine 1 is affected:

- ENGINE/1 AND 2/IGN/SYS A (49VU A03)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL

- ENGINE/IGN/ENG 1/ SYS A BAT (121VU P39)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL

- ENGINE/IGN/ENG 1/ SYS B (121VU P41)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL



C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL


C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL


C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL


12 FEB 12MEL

A320/321MEL/CDL 01.74.01

IGNITION



SEQUENCE


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7/23/2019 A 320321 Mel Cdl


74 IGNITION


ENGINE SD page

74-07-01 Selected Igniter

Indication on the

ENGINE SD page


On the EWD, check that the ENG 1(2) A+B IGN FAULT

alert is displayed.



C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH


C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH


C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH



C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH


C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH


C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH

01.74.02IGNITION


MEL



SEQUENCE


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7/23/2019 A 320321 Mel Cdl


74 IGNITION

74-09 ECAM Alert

74-09-01 ENG 1(2) IGN

A(B)(A+B) FAULT

Alert

74-09-01B One displayed C 4 3 (M) One may be displayed provided that the associated

engine ignition system is checked operative every day.


Refer to AMM 74-31-040-001

74-09-01C Two displayed C 4 2 (M) Two may be displayed provided that the associated

engine ignition systems are checked operative before

each flight.


Refer to AMM 74-31-040-001

74-31 Ignition Starting

and Continuous

Relight

74-31-01 Ignition System A

74-31-01A C 2 1 (O) One may be inoperative provided that the associated

engine ignition system B is operative.


BEFORE ENGINE START

ENGINE/1 AND 2/IGN/SYS A (49 VU A03)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL

AFTER ENGINE START

ENGINE/1 AND 2/IGN/SYS A (49 VU A03)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH

12 FEB 12MEL

A320/321MEL/CDL 01.74.03

IGNITION



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


74 IGNITION

74-31 Ignition Starting and

Continuous Relight

74-31-02 Ignition System B

74-31-02A C 2 0 (O) One or both may be inoperative.


BEFORE ENGINE START

ENGINE/IGN/ENG (1 and/or 2)/SYS B (121 VU P41/P42)

C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL

* * *

01.74.04IGNITION


MEL



SEQUENCE


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76 ENGINE CONTROLS

76-11 Throttle Control

76-11-01 Thrust lever

Position Sensor

76-11-01A A 4 3 One may be inoperative on one engine for three days

provided that:

1) The A/THR is operative, and

2) Both LGCIUs are operative, and

3) The L/G shock absorbers proximity detectors areoperative.

* * *

12 FEB 12MEL

A320/321MEL/CDL 01.76.01

ENGINE CONTROLS



SEQUENCE


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01.76.02ENGINE CONTROLS


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


77 ENGINE INDICATING


pages


CRUISE SD page

77-07-01-01 N1 Vibration

Indication on the

CRUISE SD page

77-07-01-01A Refer to Item 77-07-02-05 N1 Vibration Indication on the

ENGINE SD page


Indication on the

CRUISE SD page

77-07-01-02A Refer to Item 77-07-02-06 N2 Vibration Indication on the

ENGINE SD page

77-07-01-03 F. USED (Fuel

Used) Indication

on the CRUISESD page

77-07-01-03A Refer to Item 73-07-01 Fuel Used Indication on the

ENGINE SD page

77-07-01-04 OIL QT (Oil

Quantity)

Indication on the

CRUISE SD page

77-07-01-04A Refer to Item 79-07-03 Oil Quantity Indication on the

ENGINE SD page

12 FEB 12MEL

A320/321MEL/CDL 01.77.01

ENGINE INDICATING



SEQUENCE


I T E M

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pages


ENGINE SD page

77-07-02-01 Engine Bleed

Pressure

Indication on the

ENGINE SD

page

77-07-02-01A Refer to Item 36-07-04 Engine Bleed Precooler Inlet

Pressure Indication on the BLEED SD page

77-07-02-02 Fuel Filter Clog

Indication on the

ENGINE SD

page

77-07-02-02A Refer to Item 73-07-02 Fuel Filter CLOG Indication on the

ENGINE SD page

77-07-02-03 Fuel Used

Indication on the

ENGINE SD

page

77-07-02-03A Refer to Item 73-07-01 Fuel Used Indication on the

ENGINE SD page

77-07-02-04 Nacelle

Temperature

Indication on the

ENGINE SD

page


01.77.02ENGINE INDICATING


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




pages


ENGINE SD page


Indication on the

ENGINE SD

page

77-07-02-05A One indication

inoperative


77-07-02-05B Both indications

inoperative

A 2 0 Both may be inoperative for three flights provided that no

vibration advisory was displayed during the previous flight.


Indication on the

ENGINE SD

page

77-07-02-06A One indicationinoperative


77-07-02-06B Both indications

inoperative

A 2 0 Both may be inoperative for three flights provided that no

vibration advisory was displayed during the previous flight.

77-07-02-07 Oil Filter Clog

Indication on the

ENGINE SD

page

77-07-02-07A Refer to Item 79-07-01 CLOG Indication on the ENGINE

SD page

12 FEB 12MEL

A320/321MEL/CDL 01.77.03

ENGINE INDICATING



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




pages


ENGINE SD page

(cont’d)

77-07-02-08 Oil Pressure

Indication on the

ENGINE SD

page

77-07-02-08A Refer to Item 79-07-02 Oil Pressure Indication and

Advisory on the ENGINE SD page

77-07-02-09 Oil Quantity

Indication on the

ENGINE SD

page

77-07-02-09A Refer to Item 79-07-03 Oil Quantity Indication on the

ENGINE SD page

77-07-02-10 Oil Temperature

Indication on the

ENGINE SD

page

77-07-02-10A Refer to Item 79-07-04 Oil Temperature Indication on the

ENGINE SD page

77-07-02-11 Selected Igniter

Indication on the

ENGINE SD

page

77-07-02-11A Refer to Item 74-07-01 Selected Igniter Indication on the

ENGINE SD page



MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl




pages (cont’d)


ENGINE SD page

77-07-02-12 Start Valve

Position

Indication on the

ENGINE SD

page

77-07-02-12A Refer to Item 80-07-01 Start Valve Position Indication on

the ENGINE SD page


EWD

77-08-01 EGT Indication on

the EWD


77-08-03 Fuel Flow

Indication on the

EWD

77-08-03A Refer to Item 73-08-01 Fuel Flow Indication on the EWD

77-08-04 N1 Indication on

the EWD


77-08-05 N2 Indication on

the EWD


* * *

12 FEB 12MEL

A320/321MEL/CDL 01.77.05

ENGINE INDICATING



SEQUENCE


I T E M

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MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


78 EXHAUST


EWD

78-08-01 REV Indication on

the EWD

78-08-01A - 2 2 Both must be operative.

78-30 Thrust Reversers

78-30-01 Thrust Reverser

78-30-01A C 2 1 (O)(M)

(FD)


1) The inoperative thrust reverser is deactivated andsecured in the stowed position, and

2) All stow and deploy switches circuits on theinoperative thrust reverser are checked operative, and

3) The ENG 1(2) REV PRESSURIZED alert is notdisplayed on the EWD after deactivation, and

4) The appropriate performance adjustments are applied.


12 FEB 12MEL

A320/321MEL/CDL 01.78.01

EXHAUST



SEQUENCE


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78 EXHAUST





Performance Adjustments:

One Thrust

Reverser

Inoperative

Runway State Performance Adjustments

Takeoff Dry, or

Landing Dry, or

Landing Wet

No performance adjustments are

necessary (Basic performance data is

computed without thrust reversers)

Takeoff Wet

Use performance data computed with :

- One thrust reverser inoperative.

(Refer to SV A320/321

Performance Manual CH 12)

FOR TAKEOFF

During the takeoff briefing, the flight crew must

review:

- The status of the thrust reversers, and

- The use of the thrust reversers


01.78.02EXHAUST


MEL



SEQUENCE


I T E M

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78 EXHAUST



78-30-01A (cont’d) OPERATING PROCEDURES (cont’d)

REJECTED TAKEOFF

Ensure that both engine thrust levers are set to IDLE

detent, then:

· If one thrust reverser is inoperative:

Use both thrust levers when applying reverse thrust.

Note:

ENG (AFFECTED SIDE) REVERSER

FAULT alert is displayed on the EWD

after selection of the reverse thrust.

IN FLIGHT

· Should a failure occur with "LDG DIST

PROC.......APPLY" message displayed on the STATUS

SD page,

and

Whatever the actual thrust reversers selection at

landing:

To calculate the LDG DIST with the in-flight failure, use,

as a conservative approach, the LDG DIST factors

“WITHOUT REV” (LDG CONF/APP SPD/LDG DISTFOLLOWING FAILURES tables in the QRH part 2).


12 FEB 12MEL

A320/321MEL/CDL 01.78.03

EXHAUST



SEQUENCE


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78 EXHAUST



78-30-01A (cont’d) OPERATING PROCEDURES (cont’d)

DURING APPROACH

During the approach briefing, the flight crew must

review:

- The status of the thrust reversers, and

- The use of the thrust reversers

FOR LANDING

Before the touchdown, ensure that both engine thrust

levers are set to IDLE detent for the flare.

· After touchdown, if one thrust reverser is

inoperative:

Use both thrust levers when applying reverse thrust.

Note:

ENG (AFFECTED SIDE) REVERSER

FAULT alert is displayed on the EWD

after selection of the reverse thrust.


Refer to AMM 78-30-00-040-040

01.78.04EXHAUST


MEL



SEQUENCE


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78 EXHAUST



Inhibition Relay

sw

78-30-02A C 4 2 Two may be inoperative provided that the associated

thrust reverser is considered inoperative.

Refer to Item 78-30-01 Thrust Reverser


Shutoff Valve

78-30-03A C 2 0 One or both may be inoperative in the open position.

* * *

12 FEB 12MEL

A320/321MEL/CDL 01.78.05

EXHAUST



SEQUENCE


I T E M

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01.78.06EXHAUST


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


79 OIL


ENGINE SD page

79-07-01 CLOG Indication

on the ENGINE SD

page


79-07-02 Oil Pressure

Indication and

Advisory on the

ENGINE SD page

Note:



ENG 1(2)PUMP pb-sw FAULT light with




inoperative.


LO PR Alert


thrust reverser

checked

operative


1) The associated ENG 1(2) OIL LO PR alert isoperative, and

2) The associated oil quantity indication is operative onthe ENGINE SD page, and

3) The associated thrust reverser is checked operative.


Refer to AMM task


thrust reverser

considered

inoperative

C 2 1 One may be inoperative provided that:

1) The associated ENG 1(2) OIL LO PR alert is

operative, and2) The associated oil quantity indication is operative on

the ENGINE SD page, and

3) The associated thrust reverser is consideredinoperative.

Refer to Item 78-30-01 Thrust Reverser

12 FEB 12MEL

A320/321MEL/CDL 01.79.01

OIL



SEQUENCE


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79 OIL


ENGINE SD page

(cont’d)

79-07-03 Oil Quantity

Indication on the

ENGINE SD page

79-07-03A C 2 1 (M) One may be inoperative provided that the associated oil

quantity is checked before each flight.


Refer to AMM 79-31-00-040-042

79-07-04 Oil Temperature

Indication on the

ENGINE SD page


79-09 ECAM Alerts

79-09-01 ENG 1(2) OIL LO

PR Alert

79-09-01A C 2 0 (O) One or both may be displayed.


AFTER ENGINE START

· If both engines are affected:

RCDR GND CTL pb-sw . . . . . . . . . . . . . . . . . .CHECK ON

01.79.02OIL


MEL



SEQUENCE


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7/23/2019 A 320321 Mel Cdl


79 OIL

79-09 ECAM Alerts

79-09-02 ENG 1(2) OIL

FILTER CLOG

Alert

79-09-02B Inspection of

the visual

indicator (pop-

out) of the

electrical

master chip

detector

C 2 1 (M) One may be displayed provided that:

1) The associated filter is replaced every day, and

2) The visual indicator (pop-out) of the electrical master chip detector is checked operative before the firstMMEL dispatch, and

3) The visual indicator (pop-out) of the electrical master chip detector is inspected when the filter is replacedand does not reveal the presence of chips.


Refer to AMM 79-35-00-040-042

79-09-02C Inspection of

the electricalmaster chip

detector

C 2 1 (M) One may be displayed provided that:

1) The associated filter is replaced every day, and

2) The electrical master chip detector is inspected whenthe filter is replaced and does not reveal the presenceof chips.


Refer to AMM 79-35-00-040-044

12 FEB 12MEL

A320/321MEL/CDL 01.79.03

OIL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


79 OIL

79-20 Distribution

79-20-02 EMCD Visual Pop-

Out Indicator


79-40 IDG Oil Cooling

System

79-40-01 Fuel Return Valve

79-40-01A Refer to Item 73-10-01 Fuel Return Valve

* * *

01.79.04OIL


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


80 STARTING

80-01 ENG MAN START

Overhead Panel

80-01-31 ENG MAN START

pb-sw


80-07 Indication on the

ENGINE SD page

80-07-01 Start Valve

Position Indication

on the ENGINE SD

page

80-07-01A C 2 1 (M) One may be inoperative provided that the start valve is

checked closed after the engine start.


Refer to AMM 80-11-00-040-044

80-11 Pneumatic Starter and Valve System

80-11-01 Start Valve

80-11-01A C 2 1 (O)(M) O ne may be inoperative provided that the start valve is

manually closed after the start of the affected engine.


BEFORE ENGINE START

Refer to FCOM/PRO-SUP-70 START VALVE MANUAL

OPERATION.


Refer to AMM 80-11-00-040-045

12 FEB 12MEL

A320/321MEL/CDL 01.80.01

STARTING



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


80 STARTING

80-12 ENG MASTER Panel

on the Center

Pedestal

80-12-01 FAULT light on the

ENG MASTER

Panel


* * *

01.80.02STARTING


MEL



SEQUENCE


I T E M

7/23/2019 A 320321 Mel Cdl


ITEM PAGE

CDL INTRODUCTION

- - - - - CDL INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.01.01

LIMITATIONS

DISPATCH FUEL PENALTY

WEIGHT REDUCTIONS

SPEED CALCULATION AND RESTRICTIONS

ENROUTE DIVERSION SPEED EFFECTS

GENERAL LOCATION PICTURES & PERFORMANCE

ATA 21 - AIR CONDITIONING

21-01 Ram air inlet flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.21.01

21-03 Ram air inle leading Edge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.02

ATA 23 - COMMUNICATIONS

23-01 Static Discharger . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.23.01

ATA 27 - FLIGHT CONTROL

27-01 Flap Track Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.01

27-02 Flap Track Fairing 1A Extension . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.03

27-03 Slat Track Closing Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.04

27-05 Access Panel For Bearings At Elevator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.05

27-06 Flat Track Fairing Rear Top Cover And Tail Cone . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.06

27-07 Rubber Seal Under Slat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.07

27-08 Seal Between Inboard And Outboard Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.08

27-09 Inboard Aileron Edge To Wing Seal. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.10

27-10 Slat End Seal And Weather Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.11

27-11 Slat Track Filler Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.12

27-12 Slat Track Sealing Packer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.13

27-13 Inter-flap Cushion Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.14

27-14 Flap Track Movable Fairing Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.15

27-15 Flap Track Fixed Fairing Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.16

27-16 Flap Track Movable Fairing Pivot Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.17

27-17 Flap Tab Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.18

ATA 28- FUEL

28-01 Refuel /defuel coupling CAP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.01

28-02 Refuel Panel Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.02

12 FEB 12CDL

A320/321MEL/CDL


7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 30 - ICE AND RAIN PROTECTION

30-01 Icing indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.30.01

ATA 32 - LANDING GEAR

32-03 Nose wheel hubcap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.01

32-04 Nose fitting towing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.02

ATA 33 - LIGHTS

33-01 Wing / Engine / Scan Light Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.01

33-02 Taxi Light lamp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.02

33-03 Rear navigation light lens. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.03

33-04 Upper and lower anti-collision (Beacon) light Cover . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.04

33-05 Logo light lens (Cover) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.06

33-07 Landing light lens . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.07

33-08 Turn OFF light lamp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.08

33-09 Takeoff light lamp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.09

ATA 49 - APU

49-01 APU overpressure release door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.49.01

ATA 51- STRUCTURE

51-01 Random conductive Strip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.01

51-02 Passenger door Scuff Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.02

51-03 Bulk cargo door Scuff Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.0351-04 Fairing AFT Safety Stay Point . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.04



CDL

7/23/2019 A 320321 Mel Cdl


ITEM PAGE

ATA 52 - DOORS

52-01 Toilet sem rvicing door and drainage. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.01

52-02 Access door to hydraulic ground connectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.03

52-03 access door to potable water filling and drainage . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.05

52-04 access door to opening control of landing gear doors on ground . . . . . . . . . . . . . . . 02.52.07

52-05 access door to air conditioning ground supply. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.09

52-06 Forward jacking point access door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.11

52-07 External power ground connection access door ASSY . . . . . . . . . . . . . . . . . . . . . . . 02.52.13

52-08 Access door of cargo opening system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.14

52-09 Nose landing gear main . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.15

52-10 Nose landing gear aft doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.17

52-11 Nose landing gear leg doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.19

52-12 Main landing gear door (732, 742) (Flight with gear up) . . . . . . . . . . . . . . . . . . . . . . 02.52.21

52-13 Main landing gear door (733, 743) (Flight with gear up) . . . . . . . . . . . . . . . . . . . . . . 02.52.23

52-14 Main landing gear door (732, 742) (Flight with gear down) . . . . . . . . . . . . . . . . . . . . 02.52.25



52-18 Main landing gear door: Seal on secondary hinged fairing . . . . . . . . . . . . . . . . . . . . 02.52.31

52-19 Pax door upper cover plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.32

52-20 Access door to HP air ground connector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.33

52-21 Blue hydraulic access door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.35

52-22 Forward cargo door access cover panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.36

52-23 Aft cargo door access cover panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.37

ATA 53 - FUSELAGE

53-01 Belly Fairing Vent Louver Vanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.01

53-03 Root Fillet Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.03

ATA 54 - NACELLES / PYLON

54-01 Nacelle Strakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.01

54-03 Pylon Pressure relief door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.0354-04 Pylon Access Doors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.05

54-05 Pylon Fairing Seals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.06

54-06 Aerodynamic Seals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.07

12 FEB 12CDL

A320/321MEL/CDL

02.00.0TABLE OF CONTENT

7/23/2019 A 320321 Mel Cdl


ATA 57 - WINGS

57-01 Wing tip fences. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.01

57-02 Belly Fairing Sliding Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.03

57-03 Outboard Flaps Rubbing Strip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.04

ATA 71 - POWER PLANT

71-01 Frangible Drain Mast . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.01

71-09 Fan Cowl Hold Open Rod . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.02

ATA 78 - EXHAUST

78-09 Thrust reverser 11 and 1 O,clock Struts. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.78.01

* * *


A320/321MEL/CDL

12 FEB 12CDL

7/23/2019 A 320321 Mel Cdl


CDL Introduction

The Configuration Deviation List presented in this manual isa reproduction of the FAA-approved CDL in the Aircraft

Flight Manual (AFM). The numbering and designation of system in this CDL is based on ATA specification 100. Theparts within each systems are identified by functionaldescription, and when necessary by part number(s).

CDL General Limitations

The associated limitations for each applied CDL item mustbe listed on placard(s) affixed in the cockpit in clear view toboth pilots. The pilot in command shall be notified whenever a CDL restriction(s) exists by listing the CDL number in theflight dispatch release.

The maintenance log book briefing card must include a data

reflecting all imposed CDL(s). An appropriate inspectionnotation covering the missing part(s) must be noted onaircraft maintenance logbook before each flight.

If an additional part is lost in flight, the aircraftmay not departthe airport at which it landed following this event until it againcomplies with the appropriate CDL limitation. This, of course, does not preclude the issuance of a maintenanceferry authorization to allow the aircraft to be flown to a pointwhere the necessaryrepairs or replacements can be made.

No more than one part for any one system in this CDL maybe missing, unless specifically designated combinations areindicated.

The performance penalties are cumulative. Whereperformance penalties are listed as “NEGLIGIBLE”, nomore than three negligible items may be missing withoutapplying weight penalty. For each missing item in excess of three, the maximum performance limited weight for takeoff,enroute, and landing must be reduced by 50 kg.

Where performance penalties are not listed, anyaccumulative number of sub-systems may be missingwithout further penalty.

All CDL items must be relayed to the controlling dispatchcenter prior to departure.

Dispatch Fuel Penalty

The performance increase in the fuel must be applied to theminimum dispatch fuel requirement.

Minimum dispatch fuel required is the sum of trip fuel,alternate fuel and reserve fuel.

Weight Reductions

The MEL weight reductions must be applied to thmaximum performance limited weights, as follows:

1. Takeoff - Weight penalty is applied to the morestrictive of the Zero Wind weight o

Climb Limit weight.

2. Enroute - Weight penalty is applied to cruise an

one engine inoperative Altitud

Capability limited weights.

3. Landing - Weight penalty is applied to the mos

restrictive of tailored landing charts

field length or landing climb limite

weight.

Speed Calculation, and Restrictions

When takeoff weight penalty is imposed, determintakeoff speed with reference to the sum of actual aircragross weight plus the imposed takeoff weight penalty.

When landing weight penalty is imposed, the Vref, anthe minimum maneuvering speeds must be determinewith reference to the actual aircraft gross weight, plus thimposed landing weight penalty.

Operation with those missing item(s) requiring reduction of VMO/MMO is only permitted when th

appropriate alternate VMO set prior to flight.

Performance

Performance determination method.

There are two approved ways of determining thperformance impact on CDL items missing:

- Using CDL chapter of the Airplane Flight Manual, or- Using AFM_OCTO software.

If no performance data are available in OCTO_AFM forgiven item listed in this CDL chapter, the penaltie

published in this CDL chapter must be used.

These takeoff, en-route and landing penalties apply most limiting corresponding weight.

Takeoff and approach climb performance limiting weighare reduced by 50 kg

( Cont'd on next page )

12 FEB 12CDL

A320/321MEL/CDL

02.01.0CDL INTRODUCTIO

7/23/2019 A 320321 Mel Cdl


(Cont'd)

One engine inoperative net ceiling is reduced by 60 ft (i.e.

Corresponding to 60 kg decrease of en-route performancelimiting weight.

CAUTION

The most limiting performance between the one computedwith itemsmissing and the one computed without item missing must beused.

* * *

02.01.02CDL INTRODUCTION


CDL

7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-01 RAM AIR INLET

FLAP

2 0 All may be missing.

Note:

System performance in heating mode

will be decreased.

Performance:

The following performance penalties are applicable per

missing flap:

- Takeoff and approach climb performance limitingweights are reduced by 190 kg

- En route performance limiting weight is reduced by216 kg

- Fuel consumption is increased by 0.53 %.



SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.21.01

AIR CONDITIONING

7/23/2019 A 320321 Mel Cdl


21 AIR CONDITIONING

21-03 RAM AIR INLET

LEADING EDGE

2 1 One may be missing provided the associated pack is

turned off (Refer to MEL/MI-21-52 Air Conditioning Pack).

* * *



SEQUENCE


ITEM

02.21.02 AIR CONDITIONING


CDL

ITEM

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATION

23-01 STATIC

DISCHARGER

39 32 20 % of static dischargers may be missing or inoperative

on each the following areas:

- RH wing

- LH wing

- Vertical stabilizer (including rudder)

- RH horizontal stabilizer (including elevator)

- LH horizontal stabilizer (including elevator).

Note:

i. If a static discharger is missing or

inoperative on a flap track fairing, it

is recommended to replace it before

flight.

ii. When combined with the case of

dispatch with a wing tip fence

missing, 20 % of the remaining static

dischargers of the affected wing are

allowed to be inoperative or missing

(Refer to 57-01 Wing Tip Fence).




SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.23.01

COMMUNICATION

7/23/2019 A 320321 Mel Cdl


23 COMMUNICATION

23-01 STATIC DISCHARGER

* * *



SEQUENCE


ITEM

02.23.02COMMUNICATION


CDL

ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-01 FLAP TRACK

FAIRING

6 7 (M) One fairing may be partly or completely missing.

Note:

i. When the forward part of the fairing

is missing, the aft part must be

removed.

ii. When the aft part of the fairing is

missing, the forward part may remaininstalled.

Performance:

The following performance penalties are applicable:

- Takeoff and approach climb performance limitingweights are reduced by 1 430 kg

- En route performance limiting weight is reduced by 1575 kg


MAINTENANCE PROCEDURES

Refer to AMM 57-55-00-040-001




SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.27.01

FLIGHT CONTROL

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-01 FLAP TRACK FAIRING

(Cont’d)

02.27.02FLIGHT CONTROL


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-02 FLAP TRACK

FAIRING 1A

EXTENSION


Performance:

The following performance penalties are applicable per

missing extension:




12 FEB 12CDL

A320/321MEL/CDL 02.27.03

FLIGHT CONTROL



SEQUENCE


7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-03 SLAT TRACK

CLOSING PLATE

24 22 Two may be missing.



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-05 ACCESS PANEL

FOR BEARINGS

AT ELEVATOR

8 6 Two may be missing.

12 FEB 12CDL

A320/321MEL/CDL 02.27.05

FLIGHT CONTROL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-06 FLAP TRACK FAIRING

REAR TOP COVER

AND TAIL CONE

6 4 (M) Both may be missing on two flap track fairings.

Note:

i. When the tail cone is missing, the

rear top cover may remain installed.

ii. When the rear top cover is missing,

the associated tail cone must be

removed.


Refer to AMM 57-55-00-040-002



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-07 RUBBER SEAL

UNDER SLAT

10 0 (M) 1 m per slat may be missing.


Refer to AMM 57-40-00-040-001

12 FEB 12CDL

A320/321MEL/CDL 02.27.07

FLIGHT CONTROL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-08 SEAL BETWEEN

INBOARD AND

OUTBOARD FLAP

6 3 Three may be missing.

Note:

For dispatch with inter-flap cushion seal

missing, Refer to 27-13 Inter-flap

Cushion Seal.

Performance:


- Takeoff and approach climb performance limitingweights are reduced by 63 kg per missing seal

- En route performance limiting weight is reduced by 72kg (159 lb) per missing seal

- If two or more seals are missing, fuel consumption isincreased by 0.16 % per missing seal.




CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-08 SEAL BETWEEN

INBOARD AND

OUTBOARD FLAP

(Cont’d)

12 FEB 12CDL

A320/321MEL/CDL 02.27.09

FLIGHT CONTROL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-09 INBOARD AILERON

EDGE TO WING SEAL

4 2 One seal per aileron may be partially or completely

missing provided that any loose or flapping seal material

is cut off.



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-10 SLAT END SEAL

AND WEATHER

SEAL

12 10 One seal per wing may be partially or completely missing

provided any loose or flapping seal material is cut off.

12 FEB 12CDL

A320/321MEL/CDL 02.27.11

FLIGHT CONTROL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-11 SLAT TRACK FILLER

BLOCK


Note:

May be combined with MCDL item 27-

12 (Refer to 27-12 Slat Track Sealing

Packer).



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-12 SLAT TRACK

SEALING PACKER


Note:


11 (Refer to 27-11 Slat Track Filler

Block).

12 FEB 12CDL

A320/321MEL/CDL 02.27.13

FLIGHT CONTROL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-13 INTER-FLAP CUSHION

SEAL

4 2 One cushion seal may be missing per wing.



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-14 FLAP TRACK

MOVEABLE

FAIRING SEAL

12 6 (M) 50 % of the seal length may be missing on each side of

the flap track fairing for 100 flight hours provided that a

visual inspection is performed before each flight to ensure

there is no flapping seal on the aircraft.

Note:


15 (Refer to 27-15 Flap Track Fixed

Fairing Seal).


Refer to AMM 57-55-00-040-004

12 FEB 12CDL

A320/321MEL/CDL 02.27.15

FLIGHT CONTROL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-15 FLAP TRACK FIXED

FAIRING SEAL

18 0 (M) All may be missing provided the hole is covered with high

speed tape.

Note:


14 (Refer to 27-14 Flap Track Moveable

Fairing Seal).


Refer to AMM 57-55-00-040-004



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-16 FLAP TRACK

MOVEABLE

FAIRING PIVOT

COVER


speed tape.

Note:

A visual inspection must be performed

daily to ensure that tape is still in

position and in good condition.

12 FEB 12CDL

A320/321MEL/CDL 02.27.17

FLIGHT CONTROL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-17 FLAP TAB FAIRING 10 9 One fairing may be partly or completely missing.

Note:

i. When the forward part of the fairing

is missing, the aft part must be

removed.

ii. When the aft part of the fairing is

missing, the forward part may remain

installed.

Performance:








CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


27 FLIGHT CONTROL

27-17 FLAP TAB

FAIRING

(Cont’d)

* * *

12 FEB 12CDL

A320/321MEL/CDL 02.27.19

FLIGHT CONTROL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl





CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-01 REFUEL/DEFUEL

COUPLING CAP

101 QM OR 41 QM

2 0 (M) All may be missing provided seal integrity of coupling is

positively confirmed (i.e. no fuel leak reported).

Note:

i. If the coupling or O-ring is damaged

and the cap cannot be fitted,

dispatch is permitted in accordance

with this CDL item provided the cap

is removed and coupling integrity is

verified.

ii. If only the lanyard is missing, the

removal of the cap is not necessary.


Refer to AMM 28-25-00-040-003

* * *



SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.28.01

FUEL

7/23/2019 A 320321 Mel Cdl


28 FUEL

28-02 REFUEL PANEL DOOR 1 0 (M) Belly fairing mounted refuel panel door 192 MB may be

missing.

Note:

If belly fairing mounted refuel panel door

192 MB is not installed, underwing

mounted refuel panel doors (622KB,

522KB) must not be missing


Refer to AMM 52-42-00-040-001

* * *



SEQUENCE


ITEM

02.28.02FUEL


CDL

ITEM

7/23/2019 A 320321 Mel Cdl



30-01 ICING INDICATOR 1 0 May be missing.

Procedures:

- If icing conditions expected:

For icing conditions definition, Refer to LIM-GEN IcingConditions Definition.Turn on engine and wing anti-ice.

* * *



SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.30.01

ICE AND RAIN PROTECTION

7/23/2019 A 320321 Mel Cdl



02.30.02ICE AND RAIN PROTECTION


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-03 Nose wheel hubcap 2 1 (M) One may be missing.


Refer to AMM 32-41-00-040-001



SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.32.01

LANDING GEAR

7/23/2019 A 320321 Mel Cdl


32 LANDING GEAR

32-04 Nose Fitting Towing 1 0 (M) May be missing


Refer to AMM 32-21-00-040-001

* * *



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-01 WING/ENGINE

SCAN LIGHT

COVER 3LX, 4LX

2 1 (M) One may be missing provided the hole is covered with

high speed tape.

Note:

If non transparent high speed tape is

used, the affected light must be

deactivated (Refer to MEL/MI-33-40

Wing Scan light).



SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.33.01

LIGHTS

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-02 TAXI LIGHT LAMP 8LR 1 0 (M) May be missing provided the hole is covered with high

speed tape and the affected light is deactivated (Refer to

MEL/MI-33-40 Taxi and Takeoff light).


Refer to AMM 33-46-00-040-001

02.33.02LIGHTS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-03 REAR

NAVIGATION

LIGHT LENS 15LA

1 0 (M) May be missing for 5 flight cycles provided visual

inspection is performed before each flight to check that

there is no structural buckling.


Refer to AMM 33-41-00-040-002

12 FEB 12CDL

A320/321MEL/CDL 02.33.03

LIGHTS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-04 UPPER 7LV AND

LOWER 6LV ANTI-

COLLISION (BEACON)

LIGHT COVER

2 0 (M) All may be missing provided the lamp is covered with high

speed tape and affected light is deactivated (Refer to

MMEL/MI-33-40 Beacon light).

Performance:

If upper and lower light covers are missing, the following

performance penalties are applicable:


- En route performance limiting weight is reduced by 90kg



Refer to AMM 33-48-00-040-001


02.33.04LIGHTS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-04 UPPER 7LV AND

LOWER 6LV ANTI-

COLLISION

(BEACON) LIGHT

COVER (Cont’d)

12 FEB 12CDL

A320/321MEL/CDL 02.33.05

LIGHTS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-05 LOGO LIGHT LENS

(COVER) 3LY, 4LY


speed tape.

Note:

If non transparent high speed tape is

used, the affected light must be

deactivated.

(Refer to MEL/MI-33-40 Logo light).


Refer to AMM 33-47-00-040-001

02.33.06LIGHTS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-07 LANDING LIGHT

LENS 7LB, 8LB

2 1 (M) One may be missing provided the associated light is

retracted and deactivated and the hole is covered with

high speed tape (Refer to MEL/MI-33-40 Landing light).


Refer to AMM 33-42-00-040-001

12 FEB 12CDL

A320/321MEL/CDL 02.33.07

LIGHTS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-08 TURN OFF LIGHT

LAMP 3LC1, 3LC2



MEL/MI-33-40 Runway Turnoff light).


Refer to AMM 33-43-00-040-002

02.33.08LIGHTS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


33 LIGHTS

33-09 TAKEOFF LIGHT

LAMP 7LR

1 0 (M) May be missing provided the hole is covered with high


MEL/MI-33-40 Taxi and Takeoff light).


Refer to AMM 33-46-00-040-002

* * *

12 FEB 12CDL

A320/321MEL/CDL 02.33.09

LIGHTS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl





SEQUENCE


ITEM

02.33.10LIGHTS


CDL

ITEM

7/23/2019 A 320321 Mel Cdl


49 A PU

49-01 APU

OVERPRESSURE

RELEASE DOOR

1 0 May be missing provided APU is not used in flight and on

ground.

Limitations:

Flights for which APU is mandatory are not allowed.

* * *

12 FEB 12CDL

A320/321MEL/CDL 02.49.01

APU



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl





SEQUENCE


ITEM

02.49.02 APU


CDL

7/23/2019 A 320321 Mel Cdl


51 STRUCTURE

51-01 RADOME

CONDUCTIVE

STRIP

8 7 One may be missing.



SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.51.01

STRUCTURE

7/23/2019 A 320321 Mel Cdl


51 STRUCTURE

51-02 PASSENGER DOOR

SCUFF PLATE

4

8

0

0

All may be missing.

02.51.02STRUCTURE


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


51 STRUCTURE

51-03 BULK CARGO

DOOR SCUFF

PLATE

1 0 May be missing.

12 FEB 12CDL

A320/321MEL/CDL 02.51.03

STRUCTURE



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


51 STRUCTURE

51-04 FAIRING AFT SAFETY

STAY POINT 311 AL

1 0 May be missing.

* * *

02.51.04STRUCTURE


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-01 TOILET SERVICING

AND DRAINAGE

DOOR 172 AR

1 0 (M) May be missing.

Note:

i. Toilet system is inoperative on

ground.

ii. May be combined with MCDL items:

- 52-02 (Refer to 52-02 Access

Door to Hydraulic Ground

Connectors 197 CB - 197 EB -198 CB)


Door to Potable Water Filling

and Drainage)


Door to Opening Control of

Landing Gear Doors on Ground

195 BB - 196 BB)


Door to Air Conditioning Ground

Supply 191 CB)

- 52-06 (Refer to 52-06 Forward

Jacking Point Access Door)- 52-20 (Refer to 52-20 Access

Door to HP Air Ground

Connector 191 DB).

Performance:


- Takeoff and approach performance limiting weightsare reduced by 63 kg

En-route performance limiting weight is reduced by 72kg.




SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.52.01

DOORS

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-01 TOILET SERVICING

AND DRAINAGE

DOOR 172 AR

(Cont’d)

02.52.02DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-02 ACCESS DOOR TO

HYDRAULIC

GROUND

CONNECTORS 197

CB - 197 EB - 198 CB


Note:

May be combined with MCDL items:

- 52-01 (Refer to 52-01 Toilet

Servicing and Drainage Door )

- 52-03 (Refer to 52-03 Access Door

to Potable Water Filling and

Drainage)


to Opening Control of Landing Gear

Doors on Ground 195 BB - 196 BB)


to Air Conditioning Ground Supply

191 CB)


Jacking Point Access Door)


to HP Air Ground Connector 191

DB).

Performance:



- En-route performance limiting weight is reduced by 72kg.


12 FEB 12CDL

A320/321MEL/CDL 02.52.03

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS


HYDRAULIC

GROUND

CONNECTORS 197

CB - 197 EB - 198 CB

(Cont’d)

02.52.04DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-3 ACCESS DOOR TO

POTABLE WATER

FILLING AND

DRAINAGE 133 AL -

171 AL - 192 NB


Note:




- 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197

CB - 197 EB - 198 CB)






191 CB)



- 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191

DB).


12 FEB 12CDL

A320/321MEL/CDL 02.52.05

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS


POTABLE WATER

FILLING AND

DRAINAGE 133 AL -

171 AL - 192 NB

(Cont’d)

02.52.06DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS


OPENING CONTROL

OF LANDING GEAR

DOORS ON

GROUND 195 BB -

196 BB

2 1 One may be missing for five flight cycles.

Note:





to Hydraulic Ground Connectors 197

CB - 197 EB - 198 CB)



Drainage)



191 CB)





DB).

Limitations:

Flight in forecasted thunderstorm condition is not allowed.

Performance:



- En-route performance limiting weight is reduced by 72

kg .


12 FEB 12CDL

A320/321MEL/CDL 02.52.07

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS


OPENING CONTROL

OF LANDING GEAR

DOORS ON

GROUND 195 BB -

196 BB

(Cont’d)

02.52.08DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS


AIR CONDITIONING

GROUND SUPPLY

191 CB

1 0 May be missing.

Note:






CB - 197 EB - 198 CB)- 52-03 (Refer to 52-03 Access Door


Drainage)








DB).


12 FEB 12CDL

A320/321MEL/CDL 02.52.09

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS


AIR CONDITIONING

GROUND SUPPLY

191 CB

(Cont’d)

02.52.10DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-06 FORWARD JACKING

POINT ACCESS

DOOR

1 0 May be missing.

Note:






CB - 197 EB - 198 CB)



Drainage)






191 CB)


to HP Air Ground Connector 191DB).


12 FEB 12CDL

A320/321MEL/CDL 02.52.11

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-06 FORWARD JACKING

POINT ACCESS

DOOR

(Cont’d)

02.52.12DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-07 EXTERNAL POWER

GROUND

CONNECTION

ACCESS DOOR

ASSY 121 AL

1 0 (M) May be missing for five fl ight cycles provided the hole is

covered with high speed tape and that a visual inspection

is performed before each flight.

Limitations:

Flight in forecasted thunderstorm condition is not allowed.


Refer to AMM 52-42-00-040-003

12 FEB 12CDL

A320/321MEL/CDL 02.52.13

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-08 ACCESS DOOR OF

CARGO OPENING

SYSTEM 134 AR -

154 AR


Performance:


- Takeoff and approach climb performance limitingweights are reduced by 95 kg per missing access door

- En-route performance limiting weight is reduced by105 kg (232 lb) per missing access door

- Fuel consumption is increased by 0.21 % per missingaccess door.

02.52.14DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-09 NOSE LANDING

GEAR MAIN DOOR

(713, 714)

2 0 (M) May be missing provided both main doors (713, 714) are

removed and both aft doors (715, 716) (Refer to 52-10

Nose Landing Gear Aft Door (715, 716)) are removed.

Note:


11 (Refer to 52-11 Nose Landing Gear

Leg Door (712))

Limitations:

Passengers transportation is not allowed.

Flight with landing gear down is required.

Refer to APP-LGDN-GEN General

Maximum speed: 220 kt IAS/ M 0.5

Performance:

Note:

Reference performance for penaltiescomputations are performance with

landing gear down.



- En-route performance limiting weight is reduced by 1000 kg

- Fuel consumption is increased by 2 %.


Refer to AMM 32-22-00-040-001


12 FEB 12CDL

A320/321MEL/CDL 02.52.15

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-09 NOSE LANDING

GEAR MAIN DOOR

(713, 714)

(Cont’d)

02.52.16DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-10 NOSE LANDING

GEAR AFT DOOR

(715, 716)

2 0 (M) All may be missing.

Note:



Leg Door (712))

Limitations:



Performance:

Note:

Reference performance for penalties

computations are performance with

landing gear down.



- En-route performance limiting weight is reduced by100 kg


When combined with MCDL item 52-09 (Refer to 52-09

Nose Landing Gear Main Door (713, 714)), the

performance penalties published in 52-09 are applicable.


Refer to AMM 32-22-00-040-002


12 FEB 12CDL

A320/321MEL/CDL 02.52.17

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-10 NOSE LANDING

GEAR AFT DOOR

(715, 716)

(Cont’d)

02.52.18DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-11 NOSE LANDING

GEAR LEG DOOR

(712)


Note:

May be combined with MCDL items 52-


Main Door (713, 714)) and 52-10 (Refer

to 52-10 Nose Landing Gear Aft Door

(715, 716)).

Limitations:




Refer to AMM 32-22-00-040-003


12 FEB 12CDL

A320/321MEL/CDL 02.52.19

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-11 NOSE LANDING

GEAR LEG DOOR

(712)

02.52.20DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-12 MAIN LANDING

GEAR DOOR (732,

742) (FLIGHT WITH

GEAR UP)

2 1 (M) One may be missing.

Limitations:


Flight in forecasted icing conditions is not allowed.

Performance:


- ] Takeoff and approach climb performance limitingweights are reduced by 475 kg

- ] En-route performance limiting weight is reduced by525 kg (1 158 lb)

- ] Fuel consumption is increased by 0.96 %.


Refer to AMM 32-12-00-040-005


12 FEB 12CDL

A320/321MEL/CDL 02.52.21

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-12 MAIN LANDING

GEAR DOOR (732,

742) (FLIGHT WITH

GEAR UP)

(Cont’d)

02.52.22DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-13 MAIN LANDING

GEAR DOOR (733,

743) (FLIGHT WITH

GEAR UP)


Limitations:


Flight in forecasted icing conditions is not allowed.

Performance:






Refer to AMM 32-12-00-040-005


12 FEB 12CDL

A320/321MEL/CDL 02.52.23

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-13 MAIN LANDING

GEAR DOOR (733,

743) (FLIGHT WITH

GEAR UP)

(Cont’d)

02.52.24DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-14 MAIN LANDING

GEAR DOOR (732,

742) (FLIGHT WITH

GEAR DOWN)


Limitations:



Performance:

Note:



landing gear down.






12 FEB 12CDL

A320/321MEL/CDL 02.52.25

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-14 MAIN LANDING

GEAR DOOR (732,

742) (FLIGHT WITH

GEAR DOWN)

(Cont’d)

02.52.26DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-15 MAIN LANDING

GEAR DOOR (733,

743) (FLIGHT WITH

GEAR DOWN)


Limitations:



Performance:

Note:



landing gear down.






12 FEB 12CDL

A320/321MEL/CDL 02.52.27

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-15 MAIN LANDING

GEAR DOOR (733,

743) (FLIGHT WITH

GEAR DOWN)

(Cont’d)

02.52.28DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-16 MAIN LANDING

GEAR DOOR (734,

744) (FLIGHT WITH

GEAR DOWN)


Limitations:



Performance:

Note:



landing gear down.






12 FEB 12CDL

A320/321MEL/CDL 02.52.29

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-16 MAIN LANDING

GEAR DOOR (734,

744) (FLIGHT WITH

GEAR DOWN)

(Cont’d)

02.52.30DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-18 MAIN LANDING

GEAR DOOR : SEAL

ON SECONDARY

HINGED FAIRING


Performance:

If three or more seals are missing, the following

performance penalties are applicable:

- Takeoff and approach climb performance limitingweights are reduced by 24 kg per missing seal

- En-route performance limiting weight is reduced by 27

kg per missing seal

- Fuel consumption is increased by 0.07 % per missingseal.

12 FEB 12CDL

A320/321MEL/CDL 02.52.31

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-19 PAX DOOR UPPER

COVER PLATE


Note:

The affected door must be considered

as inoperative (Refer to MEL/MI-52-10

Cabin Passenger Door).

Performance:

The following performance penalties are applicable:- Takeoff and approach climb performance limiting

weights are reduced by 79 kg per missing plate

- En-route performance limiting weight is reduced by 88kg (195 lb) per missing plate

- If 2 or more plates are missing, fuel consumption isincreased by 0.18 % per missing plate.

02.52.32DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS


HP AIR GROUND

CONNECTOR 191

DB

1 0 (M) May be missing for ten flight cycles.

Note:






CB - 197 EB - 198 CB)



Drainage)






191 CB)


Jacking Point Access Door).


Refer to AMM 47-20-00-040-002


12 FEB 12CDL

A320/321MEL/CDL 02.52.33

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS


HP AIR GROUND

CONNECTOR 191

DB

(Cont’d)

02.52.34DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-21 BLUE HYDRAULIC

ACCESS DOOR 197

FB



Refer to AMM 52-41-00-040-001

12 FEB 12CDL

A320/321MEL/CDL 02.52.35

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-22 FORWARD CARGO

DOOR ACCESS

COVER PANEL 825

AR

1 0 (M) May be missing provided all latching hooks are checked

latched and locked before each flight.

Performance:



- En-route performance limiting weight is reduced by

266 kg


02.52.36DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


52 DOORS

52-23 AFT CARGO DOOR

ACCESS COVER

PANEL 826 AR

1 0 (M) May be missing provided all latching hooks are checked

latched and locked before each flight.

Performance:



- En-route performance limiting weight is reduced by

216 kg


* * *

12 FEB 12CDL

A320/321MEL/CDL 02.52.37

DOORS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl



02.52.38DOORS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


53 FUSELAGE

53-01 BELLY FAIRING

VENT LOUVER

VANE

24 18 (M) Three may be missing per vent louver.

Note:

Vane with a crack length higher than

50% must be removed before next flight.



SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.53.01

FUSELAGE

7/23/2019 A 320321 Mel Cdl


53 FUSELAGE

53-03 ROOT FILLET

FAIRING


Note:

Must not be combined with MCDL item

54-01 (Refer to 54-01 Nacelle Strake) or

MCDL item 54-03 (Refer to 54-03 Pylon

Pressure Relief Door 413(423) BL -

414(424) BR).

Performance:

The following performance penalty is applicable:

- Takeoff performance limiting weight is reduced by 900kg.

Note:

The above performance penalty is not

applicable if the flight crew can check

V2 greater than 1.15 VS1G.




SEQUENCE


ITEM

02.53.02FUSELAGE


CDL

ITEM

7/23/2019 A 320321 Mel Cdl


53 FUSELAGE

53-03 ROOT FILLET

FAIRING

(Cont’d)

* * *

12 FEB 12MEL

A320/321MEL/CDL 02.53.03

FUSELAGE



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl



02.53.04FUSELAGE


MEL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


54 NACELLES / PYLON

54-01 NACELLE STRAKE 4 0 All may be missing.

Note:

Must not be combined with MCDL item

53-03 (Refer to 53-03 Root Fillet

Fairing).

Procedures:

Approach speed: VLS + 4 kt.

Landing distance: multiply by 1.09.

Performance:


- If no internal strakes and one or both external strakesare missing, takeoff performance limiting weight isreduced by 2 380 kg

- If one or both internal strakes are missing (with or without external strakes missing), takeoff performancelimiting weight is reduced by 3 270 kg

- Increase V2 and VR by 1 kt.

Note:

The performance penalties are not

applicable if the flight crew can check

V2 greater than 1.17 VS1G.




SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.54.01

NACELLES / PYLON

7/23/2019 A 320321 Mel Cdl


54 NACELLE / PYLON

54-01 NACELLE STRAKE

(Cont’d)

02.54.02NACELLES / PYLON


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


54 NACELLES / PYLON

54-03 PYLON

PRESSURE

RELIEF DOOR

413(423) BL -

414(424) BR

4 0 (M) All may be missing for 5 fl ight cycles only.

Note:

i. If one door is missing on a pylon, the

other door on the same pylon must

be removed.

ii. Must not be combined with MCDL

item 53-03 (Refer to 53-03 Root

Fillet Fairing).

Limitations:

Maximum cruise speed: M 0.78.

Procedures:

Approach speed: VLS + 4 kt.

Landing distance: multiply by 1.09.

Performance:


- Takeoff performance limiting weight is reduced by 2380 kg

- Increase V2 and VR by 1 kt

Note:

The above performance penalties are

not applicable if the flight crew can

check V2 greater than 1.16 VS1G.

- If two or more doors are missing, en routeperformance limiting weight is reduced by 40 kg per missing door

- If three or more doors are missing, fuel consumption isincreased by 0.09 % per missing door.


Refer to AMM 54-52-00-040-001


12 FEB 12CDL

A320/321MEL/CDL 02.54.03

NACELLES / PYLON



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


54 NACELLES / PYLON

54-03 PYLON PRESSURE

RELIEF DOOR

413(423) BL -

414(424) BR

(Cont’d)



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


54 NACELLES / PYLON

54-04 PYLON ACCESS

DOOR 415(425) AL

- 415(425) AR

4 0 All may be missing for 5 flight cycles provided the hole is

covered with high speed tape.

Limitations:

Flight in forecasted thunderstorm conditions is not

allowed.

12 FEB 12CDL

A320/321MEL/CDL 02.54.05

NACELLES / PYLON



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


54 NACELLES / PYLON

54-05 PYLON FAIRING

SEAL

4 3 One may be missing per pylon.



CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


54 NACELLE/PYLON

54-06 AERODYNAMIC

SEAL



Refer to AMM 54-53-00-040-001

12 FEB 12MEL

A320/321MEL/CDL 02.54.07

NACELLES / PYLON



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl





MEL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


57 WINGS

57-01 Wing Tip Fence

57-01a Lower Part Of A

Wing Tip Fence

2 1 (M) One lower part of a wing tip fence may be missing

provided the broken part is removed and holes are

covered.

Performance:






Refer to AMM 57-31-00-040-001

57-01b Complete Wing Tip

Fence

2 1 (M) One complete wing tip fence may be missing provided

exposed interior structure is covered, protective material

is inspected before each flight and replaced if necessary.

Performance:






Refer to AMM 57-31-00-040-001




SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.57.01

WINGS

7/23/2019 A 320321 Mel Cdl


57 WINGS

57-01 Wing Tip Fence

(Cont’d)

02.57.02WINGS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


57 WINGS

57-02 BELLY FAIRING

SLIDING PANEL


Performance:

If two panels are missing, the following performance

penalties are applicable:


- En route performance limiting weight is reduced by

108 kg- Fuel consumption is increased by 0.28 %.

12 FEB 12CDL

A320/321MEL/CDL 02.57.03

WINGS



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


57 WINGS

57-03 OUTBOARD FLAP

RUBBING STRIP

ITEMS 40, 70, 80, 85,

100, 120


* * *

02.57.04WINGS


CDL



SEQUENCE


ITEM

7/23/2019 A 320321 Mel Cdl


71 POWER PLANT

71-01 FRANGIBLE

DRAIN MAST

2 0 ((M) All may be missing.


Refer to AMM 71-71-42-040-044



SEQUENCE


ITEM

12 FEB 12CDL

A320/321MEL/CDL 02.71.01

POWER PLANT

7/23/2019 A 320321 Mel Cdl


71 POWER PLANT

71-09 FAN COWL HOLD

OPEN ROD



Refer to AMM 71-13-12-000-040

02.71.02POWER PLANT


CDL



SEQUENCE


ITEM

a 320321 mel cdl

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