halaman ganjil

8/9/2019 halaman ganjil

1/38

N: New

R: Revised

D:

Deleted

Chap Sect

TITLE

LOEP

LOEP

LOEP

LOEP

LOEP

LOEP

LOEP

TOG

TOG

TOG

HIGHLIGHTS

HIGHLIGHTS

SB LIST

INTRO

INTRO

INTRO

INTRO

lr\ITRO

INTRO

lf\ITRO

INTRO

INTRO

lf\ITRO

GLOSSARY

HOW TO USE

HOW TO USE

HOW TO USE

HOW TO USE

OPTIONAL

OPTIONAL

OPTIONAL

OPTIONAL

O ~ : i - 1 0 GENE

O ~ : i 1 0 GENE

0 ~ > - 1 0 TABLE

O ~ : i - 1 0 TABLE

O ~ : i 1 0 00 REP

0 ~ - 1 0 00 REP

O ~ : i 1 0 00

ATA

21 52

Ot:i 1 0 00

ATA

21 53

0 ~ 5 1 0 00 ATA 22 30

Page

1

2

3

4

5

6

7

1

2

3

1

2

1

1

2

3

4

5

6

7

8

9

10

1

1

2

3

4

1

2

3

4

1

2

1

2

1

2

1

1

1

M INTEN NCE PROGR M

LIST OF EFFE TIVE P GES

Type Date Chap Sect Page Type

Date

N

2012.07.02

05 10 00

ATA

22 30

2 2011.06.09

N 2012.07.02

05 10 00

ATA

23 52 1

2009.05.14

N

2012.07.02

05 10 00 ATA 23 71 1

2010.10.11

N

2012.07.02

05 10 00 ATA 24 20 1 2010.10.11

N 2012.07.02 . 05 10 00

ATA

24 20 2 2010.10.11

N 2012.07.02

05 10 00

ATA

24 30 1 2003.01.03

N

2012.07.02

05 10 00

ATA

24 31 1 2007.01.09

N

2012.07.02

05 1 0 00

ATA

25 00 1

2008.01.28

N

2012.07.02

05 10 00

ATA

25 10 1

2005.04.21

N

2012.07.02 05 10 00

ATA

25 62 1

2006.04.07

N 2012.07.02

05 10 00

ATA

25 62 2

2006.04.07

N

2012.07.02

05 10 00 ATA 25 64 1

2007.04.30

N

2012.07.02

05 10 00 ATA

25 64

2 2007.04.30

2012.03.22

05 10 00

ATA

25 64

3

2007.04.30

2012.03.22

05 10 00

ATA

25 64 4

2007.04.30

2012.03.22

05 10 00

ATA

25 64

5

2007.04.30

2012.03.22

05 10 00

ATA

25 64

6

2007.04.30

2012.03.22

05 10 00

ATA

25 64 7 2007.04.30

2012.03.22

05 10 00

ATA

25 66

1

2012.03.22

2012.03.22

05 10 00 ATA

25 66

2 2012.03.22

2012.03.22

05 10 00 ATA 25 66

3

2012.03.22

2012.03.22

05 10 00 ATA 25 66 4 2012.03.22

2012.03.22

05 10 00

ATA

25 66

5

2012.03.22

2012.03.22

05 10 00

ATA

25 66

6

2012.03.22

2004.03.25

05 10 00

ATA

25 69

1 2008.09.01

2006.04.07

05 10 00 ATA 25 69 2 2008.09.01

2006.04.07

05 10 00 ATA 25 69

3

2008.09.01

2006.04.07

05 10 00 ATA 25 81

1 2007.01.09

2006.04.07

05 10 00 ATA 25 81

2

2007.01.09

2003.01.03

05 10 00 ATA 26 13 1 2003.01.03

2003.01.03

05 10 00

ATA

26 21 1 R 2012.07.02

2003.01.03

05 10 00 ATA 26 21

2 R 2012.07.02

2003.01.03

05 10 00 ATA 26 22 1

2005.04.21

2012.03.22

05 10 00 ATA 28 10 1 2011.06.09

2012.03.22

05 10 00

ATA

28 20 1 2011.06.09

2004.03.25

05 10 00 ATA 28 20 2 2011.06.09

2004.03.25

05 10 00

ATA

28 41 1 2008.09.01

N

2012.07.02

05 10 00 ATA 28 93 1

2003.01.03

N

2012.07.02

05 1 0 00 ATA 29 1 0

1 2010.10.11

2007.01.09

05 10 00 ATA 29 10 2 2010.10.11

2008.01.28

05 10 00 ATA 29 10 3

2010.10.11

2011.06.09

05 10 00 ATA 29 10

4

2010.10.11


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~ J : 1 9 C O P T E R

M INTEN NCE

PROGR M

Chap Sect

Page

Type

Date

Chap Sect

Page

Type Date

05 20 01

ATA

28 10 1 2006.04.07 05 20 01

ATA

36 10 1 2004.03.25

05 20 01

ATA

28 11

1

R

2012.07.02

05 20 01

ATA

36 10 2

2004.03.25

05 20 01

ATA

28 20

1

2009.05.14

05 20 01 ATA 39 11

1 2003.01.03

05 20 01 ATA 28 30

1

2003.01.03

05 20 01 ATA 45 11

1

2010.10.11

05 20 01 ATA 28 40

1

2008.09.01

05 20 01 ATA

45 11

2

2010.10.11

05 20 01 ATA 28 41

1

2003.01.03

05 20 01 ATA 47 50

1

2011.06.09

05 20 01 ATA 28 91

1

2003.01.03

05 20 01 ATA 52 10

1

2003.01.03

05 20 01 ATA 28 92

1

2003.01.03

05 20 01

ATA 52 11

1 2012.03.22

05 20 01 ATA 28 93

1

2003.01.03

05 20 01 ATA52 11

2

2012.03.22

05 20 01 ATA 29 00

1

2005.04.21

05 20 01 ATA 52 12

1

2003.01.03

05 20 01 ATA 29 10

1

2005.04.21

05 20 01 ATA 52 13

1

2003.01.03

05 20 01 ATA 29 10

2

2005.04.21

05 20 01 ATA 52 14

1

2003.01.03

05 20 01 ATA 29 20

1

2003.01.03

05 20 01 ATA 52 30

1

2003.01.03

05 20 01

ATA

30 20

1

2011.06.09

05 20 01 ATA 53 00

1

2011.06.09

05 20 01 ATA 30 20

2

2011.06.09

05 20 01 ATA 53 00

2

2011.06.09

05 20 01

ATA

30 20 3

2011.06.09

05 20 01 ATA 53 10

1

2011.06.09

05 20 01

ATA

30 30

1

2003.01.03

05 20 01

ATA

53 10

2

2011.06.09

05 20 01 ATA 30 41

1

2003.01.03

05 20 01 ATA 53 10

3

2011.06.09

05 20 01 ATA 30 42

1

2012.03.22

05 20 01 ATA 53 10

4

2011.06.09

05 20 01 ATA 30 60

1

2007.09.20

05 20 01 ATA 53 20

1

2004.03.25

05 20 01 ATA 30 60

2

2007.09.20

05 20 01 ATA 53 40

1

2005.04.21

05 20 01 ATA 30 61

1

2003.01.03

05 20 01

ATA

53 40

2

2005.04.21

05 20 01 ATA 30 80

1

2007.01.09

05 20 01 ATA 53 50

1

2011.06.09

05 20 01 ATA 31 32

1

2008.09.01

05 20 01 ATA 53 50

2

2011.06.09

05 20 01 ATA 31 32

2

2008.09.01

05 20 01 ATA 55 10

1

R

2012.07.02

05 20 01

ATA

31 50 1 2003.01.03 05 20 01

ATA

55 10 2

R

2012.07.02

05 20 01 ATA 32 00

1

2003.01.03

05 20 01 ATA 56 10

1

2003.01.03

05 20 01 ATA 32 12

1

2003.01.03

05 20 01 ATA 56 20

1

2008.09.01

05 20 01 ATA 32 22

1

2003.01.03

05 20 01 ATA 62 10

1

2011.06.09

05 20 01 ATA 32 30

1

2010.10.11

05 20 01 ATA 62 10

2

2011.06.09

05 20 01 ATA 32 30

2

2010.10.11

05 20 01 ATA 62 10 3

2011.06.09

05 20 01 ATA 32 30 3

2010.10.11

05 20 01 ATA 62 10

4

2011.06.09

05 20 01

ATA

32 40

1

2010.10.11

05 20 01 ATA 62 10

5

2011.06.09

05 20 01 ATA 32 40

2

2010.10.11

05 20 01 ATA 62 10 6

2011.06.09

05 20 01

ATA

32 50

1

2003.01.03

05 20 01 ATA 62 10

7

2011.06.09

05 20 01 ATA 32 70

1

2003.01.03

05 20 01 ATA 62 35

1

2012.03.22

05 20 01 ATA 32 91

1

2008.01.28

05 20 01 ATA 62 35

2

2012.03.22

05 20 01 ATA 33 10

1

2003.01.03

05 20 01 ATA 62 35 3

2012.03.22

05 20 01

ATA

33 20 1 2003.01.03 05 20 01

ATA

62 35 4 2012.03.22

05 20 01

ATA

33 40

1

2003.01.03

05 20 01 ATA 62 35

5

2012.03.22

05 20 01 ATA 33 43

1

2007.09.20

05 20 01 ATA 62 35 6

2012.03.22

05 20 01

ATA

33 43

2

2007.09.20

05 20 01 ATA 62 36

1

2006.04.07

05 20 01 ATA 33 45

1

2008.09.01

05 20 01 ATA 62 36

2

2006.04.07

05 20 01 ATA34 11

1

R

2012.07.02

05 20 01 ATA 63 10

1

2012.03.22

05 20 01 ATA 34 21

1

2003.01.03

05 20 01 ATA 63 20

1

2012.03.22

05 20 01 ATA 34 22

1

2003.01.03

05 20 01 ATA 63 20

2

2012.03.22

05 20 01

ATA

34 23

1

2003.01.03

05 20 01 ATA 63 20

3

2012.03.22

05 20 01 ATA 34 42

1

2011.06.09

05 20 01 ATA 63 21

1

2005.04.21

05 20 01 ATA 34 42

2

2011.06.09

05 20 01 ATA 63 23

1

2011.06.09

05 20 01

ATA

35 30

1

2009.05.14

05 20 01 ATA 63 23

2

2011.06.09


3/38

~ Y R 9 C O P T E R

MAINTENANCE PROGRAM

Chap/Sect

Page

Type

Date

Chap/Sect

Page

Type

Date

05 20 02

5

H 5 R 2012.07.02 05 20 02 2000 H 1 2007.09.20

05 20 02 500 H

6

R

2012.07.02

05 20 02 2000 H

2

2007.09.20

05 20 02 500 H

7 R

2012.07.02

05 20 02 2500 H

1

2010.10.11

05 20 02 500 H

8

R

2012.07.02

05 20 02 3000 H

1

2008.09.01

05 20 02 500 H

9

R

2012.07.02

05 20 02 3000 H

2

2008.09.01

05 20 02 500 H

1

R

2012.07.02

05 20 02 3000 H

3

2008.09.01

05 20 02 500 H

R

2012.07.02

05 20 02 3000 H

4

2008.09.01

05 20 02 500 H

12 R

2012.07.02

05 20 02 3500 H

1

2012.03.22

05 20 02 500 H

13

R

2012.07.02

05 20 02 3750 H

1

2003.01.03

05 20 02 500 H

14

R

2012.07.02

05 20 02 4500 H

1

2010.10.11

05 20 02 500 H

15

R

2012.07.02

05 20 02 7500 H

1

2011.06.09

05 20 02 500 H

16

R

2012.07.02

05 20 02 7500 H

2

2011.06.09

05 20 02 500 H

17

R

2012.07.02 05 20 02 7500 H

3

2011.06.09

05 20 02 500 H

18

R

2012.07.02

05 20 02 7500 H

4

2011.06.09

05 20 02 500 H

19

R

2012.07.02

05 20 02 7500 H

5

2011.06.09

05 20 02 500 H

2

R

2012.07.02

05 20 02 7500 H

6

2011.06.09

05 20 02 500 H

21

R

2012.07.02

05 20 02 7500 H

7

2011.06.09

05 20 02 500 H

22

R

2012.07.02

05 20 02 7500 H

8

2011.06.09

05 20 02 500 H

23

R

2012.07.02

05 20 02 7500 H

9

2011.06.09

05 20 02 500 H

24

R

2012.07.02

05 20 02 7500 H

1

2011.06.09

05 20 02 500 H

25

R

2012.07.02

05 20 02 7500 H

2011.06.09

05 20 02 500 H

26

R

2012.07.02

05 20 02 7500 H

12

2011.06.09

05 20 02 500 H

27

R

2012.07.02

05 20 02 7500 H

13

2011.06.09

05 20 02 500 H

28

R

2012.07.02

05 20 02 7500 H

14

2011.06.09

05 20 02 500 H

29

R

2012.07.02

05 20 02 7500 H

15

2011.06.09

05 20 02 500 H 30 R 2012.07.02 05 20 02 7 D 1 2004.03.25

05 20 02

5

H

31

R

2012.07.02

05 20 02 7 D

2

2004.03.25

05 20 02 500 H

32

R

2012.07.02

05 20 02 8 D

1

2003.01.03

05 20 02 500 H

33

R

2012.07.02

05 20 02 1 M

1

2011.06.09

05 20 02 500 H

34

R

2012.07.02

05 20 02 1 M

2

2011.06.09

05 20 02 500 H

35

R

2012.07.02

05 20 02 1 M

3

2011.06.09

05 20 02 500 H

36

R

2012.07.02

05 20 02 2 M

1

2011.06.09

05 20 02 500 H

37

R

2012.07.02

05 20 02 2 M

2

2011.06.09

05 20 02 500 H

38

R

2012.07.02

05 20 02 2 M

2011.06.09

05 20 02 500 H

39

R

2012.07.02

05 20 02 3 M

1

2009.05.14

05 20 02 500 H

4

R

2012.07.02

05 20 02 3 M

2

2009.05.14

05 20 02 520 H

1

2003.01.03

05 20 02 6 M

1

2011.06.09

05 20 02 550 H

1

2008.09.01

05 20 02 6 M

2

2011.06.09

05 20 02 600 H

1

2005.04.21 05 20 02 6 M 3 2011.06.09

05 20 02 800 H

1

2003.01.03

05 20 02 6 M

4

2011.06.09

05 20 02 800 H

2

2003.01.03

05 20 02 6 M

5

2011.06.09

05 20 02 1000 H

1

R

2012.07.02

05 20 02 6 M

6

2011.06.09

05 20 02 1000 H

2

R

2012.07.02

05 20 02 6 M

7

2011.06.09

05 20 02 1000 H

R

2012.07.02

05 20 02 6 M

8

2011.06.09

05 20 02 1000 H

4

R

2012.07.02

05 20 02 6 M

9

2011.06.09

05 20 02 1500 H

1

2010.10.11

05 20 02 6 M

1

2011.06.09

05 20 02 1500 H

2

2010.10.11

05 20 02 1 y

1

2010.10.11

05 20 02 1500 H

3

2010.10.11

05 20 02 1 y

2

2010.10.11

05 20 02 1500 H

4

2010.10.11

05 20 02 1 y

3

2010.10.11

05 20 02 1500 H

5

2010.10.11

05 20 02 1

y

4

2010.10.11


4/38

M INTEN NCE PROGR M

Chap Sect

Page

Type

Date Chap Sect

Page Type

Date

05 20 03

T

62 35 3 2011.06.09

05 20 03

T

62 36 1

2003.01.03

05 20 03

T

63 20

1

2006.04.07

05 20 03 T 63 20

2

2006.04.07

05 20 03

T

63 25 1

2005.04.21

05 20 03

T

63 28

1

2005.04.21

05 20 03

T

63 30 1

2003.01.03

05 20 03

T

64 10

1

2003.01.03

05 20 03

T

64 20 1

2007.04.30

05 20 03 T 64 20

2 2007.04.30

05 20 03 T 64 20

3

2007.04.30

05 20 03 T 65 10 1

2004.03.25

05 20 03

T

65 20

1 2007.04.30

05 20 03 T 65 20

2

2007.04.30

05 20 03

T

67 30 1

2007.09.20

05 50 GENE 1

2003.01.03

05 50 00 REP 1 N 2012.07.02

05 50 00 T 28 20 1

2003.01.03

05 50 00 T 28 93 1 2003.01.03

05 50 00

T

30 20

1 2007.09.20

05 50 00

T

30 61

1 2003.01.03

05 50 00

T

32 70

2003.01.03

05 50 00 T 33 20

2003.01.03

05 50 00 T 62 10

R

2012.07.02

05 50 00

T

62 36

1 2003.01.03

05 50 00

T

63 23 1 2005.04.21

05 50 00 T 64 10

1 R 2012.07.02

05 50 00

T

65 10 1 2005.04.21


5/38

~ - B 9 C O P T E R

M INTEN NCE

PROGR M

TABLE OF CONTENTS

Title age

TRANSMITIAL

L IT R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

1 INSTRUCTIONS ...........................................................................................

2 OUTLINE OF THE REVISION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

3 DETAILED DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

LIST OF SERVICE BULLETINS INCORPORATED

.. .. .. . .. .. .. .. .. .. .. . .. .. .. . .. .. .. .. .. .. .. ..

INTRODUCTION

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

GENERAL ..................................................................................................

1 1

Scope of the Maintenance Program

...........................................................

1.2 Classification of the information

.................................................................

1 3

Airworthiness Limitations .........................................................................

1.4

Adaptation of the PRE by the Operator .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. 2

1 5

Changes

in

the PRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

1.6 Feedback

of

Information from the Operator to the Manufacturer . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

1 7 Effectivity - Responsibility . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

2 DEFINITIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

2 1 Aircraft Maintenance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

2.2 Types of Maintenance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

2 2 1 PREVENTIVE MAINTENANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

2.2.2 CORRECTIVE MAINTENANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

2.2.3 REMEDIAL MAINTENANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

2.3 Maintenance Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

2 3 1 Hard Time Maintenance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

2.3.2

On

Condition Maintenance: OC ( On Condition ) or CHK ( Inspection Check ) . . . 4

2.3.3 Condition Monitoring . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

2.4 Particular and Severe Operating Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

2 4 1 Definitions: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

2.5 Maximum compliance interval for maintenance operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

2 5 1 Definition of the margins .. .. . .. .. .. .. .. .. . .. .. . .. . .. . .. .. .. .. .. .. . .. .. . .. .. . .. .. .. . .. .. .. 6

2.5.1.1 lntetals classified as 2-star intervals .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. . 6

2.5.1.2

lnte als

classified

as

1-star intervals .. .. .. .. . .. .. . .. .. . .. .. .. .. .. .. .. .. . .. . 7

2.5.22 5 1 ~ u m m a ~ t ~ r ~ ~ ~ ~ ~ ~ ~ . ~ i ~ i . ~ ~ . ~ ~ . ~ ~ ~ ~ . ~ ~ ~ . ~ . ~ i ~ ~ .. ~ ~ ~ ~ t . ~ ~ : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : :

2.5.3 Use of the margins . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

2.6 Authorization to

in

tall and transfer a component (part or assembly) from one aircraft

version to another aircraft version . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

2 6 1

Components not Subject to In-Service Monitoring .. . .. .. .. .. . .. .. .. . .. . .. .. .. .. .. .. .. 9

2.6.2 Components Subject to In-Service Monitoring .. .. .. .. .. .. . .. . .. .. .. .. . .. .. ..

..

.

.. ..

.. . 9

2.6.2.1 Transfer Authorization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

2.6.2.2 Components Subject to a Service Life Limit (SLL) . . . . . . . . . . . . . . . . . . . . . . . . . . 9

2.6.2.3 Components Subject to an Operating Time Limit (OTL) . . . . . . . . . . . . . . . . . . . . . 9


6/38

~ 1 9 C O P T E R

MAINTENANCE PROGR M

Title

Page

1 INTRODUCTION

2

PRESENTATION OF THE INFORMATION

3

AIRCRAFT MAINTENANCE

3 1 Scheduled Maintenance Operations Classified by Chapter/Section: Section 05 20 01 2

3 2

Scheduled Maintenance Operations Classified according to the Recommended Inspection

Schedule: Section

05 20 02 2

3 3

Unscheduled Maintenance Operations e.g. : After Component Replacement) : Section

05 20 03 2

3 4

Daily Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

3

3 5

Additional Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

3

3 6

Basic Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

3

3.7 Major Inspection G) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

4

MARGINS APPLICABLE TO MAINTENANCE INTERVALS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

5

05 20 HOW TO US THE TABLES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

GENERAL PRESENTATION

2

DESCRIPTION

3

DOCUMENTATION

4

LIMIT

5

CL 1

05 50 SPECIAL MONITORING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

GENERAL


7/38

~ - 3 9 C O P T E R

M INTEN NCE PROGR M

TR NSMITT L LETTER

1 INSTRUCTIONS

- Check that the content of the sections is in accordance with the List of Effective Pages .

- Return the acknowledgment card.

2 OUTLINE O THE REVISION

The revision is codified as follows:

- Revision

013

frozen: 2012.07.02.

3 DETAILED DESCRIPTION

Section 05-10-00

ATA 26 21 ENGINE FIRE EXTINGUISHERS

- Modification of date code without technical modification.

Section 05-20-01/02 The scheduled maintenance operations)

ATA 26 21

ENGINE FIRE EXTINGUISHERS

~ - Modification

of

date code without technical modification.

ATA 28 11

OPT - PRESSURE REFUELLING

- 28/11/00/000/000/000

PRESSURE REFUELLING SYSTEM

Description

and

documentation modified: MET 28.11.00.503 added.

ATA 34 11 PITOT-STATIC SYSTEM INSTRUMENTS

- 34/11/00/601/000/010

AIR DATA SYSTEM

New task integrated.

ATA 55-10 HORIZONTAL STABILIZER

500 H

500 H//2 Y


8/38

~ 3 _ 9 C O P T E R

MAINTENANCE PROGR M

TR NSMITT L LETTER

1 INSTRUCTIONS

- Check that the content of the sections is in accordance with the List of Effective Pages .

- Return the acknowledgment card.

2 OUTLINE OF THE REVISION

The revision is codified as follows:

- Revision 012 frozen: 2012.03.22.

3 DETAILED DESCRIPTION

Section

SB

LIST

- Addition of service bulletins:

SB 05.00.88: TIME LIMITS - MAINTENANCE CHECKS - ICE AND RAIN PROTECTION -

De-icing system slip-ring ATA 30-60).

SB

05.00.90: TIME LIMITS - MAINTENANCE CHECKS - Changes to the maintenance intervals

of transformer-rectifiers MP/N 684-1009-200 ATA 24-30 and ATA 25-64).

Section INTRO

- Paragraph

2.6.2.1

modified.

Section 05 10 GENE

- Paragraph modified.

Section 05 1 0 00

ATA

25-66 OPT - EMERGENCY LOCATOR TRANSMITTER

- 25/66/00/000/000/115

B T T E R ~ RECHARGEABLE

Description modified.

ATA 30-60 OPT - DE-ICING SYSTEM

OTL 4 Y


9/38

~ ~ Q O P T E R

MAINTENANCE PROGR M

25/64/02/000/000/11 0

EMERGENCY ELECTRICAL HOIST TRANSFORMER RECTIFIER

Documentation modified.

3500 H//6 Y

ATA 25 69 OPT LIFE RAFTS

25/69/1 0/602/000/000

SPONSON MOUNTED LIFE RAFT

Title and documentation modified.

25/69/10/602/000/010

SPONSON MOUNTED LIFE RAFT

New task integrated.

ATA 26 11 ENGINE FIRE DETECTION

26/11

/00/501 /000/01 0

FIRE DETECTION


ATA 30 42 WINDSHIELD WIPERS

30/42/00/602/000/000

MOTOR BRUSHES

Task deleted.

ATA

34 11

PITOT STATIC SYSTEM INSTRUMENTS

34/11

/00/601 /000/01 0

STATIC PRESSURE VALVE

Task deleted.

ATA

52 11

SIDE DOORS

52/11 /01 /602/000/000

SIDE PLUG DOOR


ATA 62 35 MAIN ROTOR HUB/SHAFT

62/35/00/000/000/115

MAIN ROTOR HEAD/MAST


62/35/00/000/000/120

MAIN ROTOR HEAD/MAST


500 H

500 H

500 H

2 y

500 H

250 H

y

Y


10/38

~ Q C O P T E R

65 1 0 00 000 000 340

TAIL ROTOR DRIVE


65 1

0/00/000/000/350

TAIL ROTOR DRIVE


65 1 0/00/000/000/360

TAIL ROTOR DRIVE


ATA 65 20 INTERMEDIATE GEARBOX

65/20/00/601/000/020

INTERMEDIATE GEARBOX


65/20/00/601/000/030



65/20/00/601/000/040



MAINTENANCE PROGR M

Y

Y

y

Y

Y

y


11/38

-: B9COPTER

M INTEN NCE PROGR M

No

01.00.45

05.00.44

05.00.46

05.00.47

05.00.48

25.00.79

63.00.58

05.00.62

05.00.61

30.00.56

05.00.30

05.00.69

05.00.75

05.00.79

05.00.83

25.02.11

30.00.56

34.00.40

05.00.82

05.00.86

63.00.68

64.00.31

05.00.88

05.00.90

LIST OF SERVICE BULLETINS INCORPOR TED

Frozen revision

date

Subject

2006.04.07

2007.04.30

2007.04.30

2007.09.20

2008.09.01

2010.10.11

2010.10.11

2010.10.11

2010.10.11

2010.10.11

2010.10.11

2010.10.11

2010.10.11

2011.06.09

2012.03.22

2012.03.22

Main rotor blades leading edge inspection (superseded by

SB No.

05.00.46)

ATA

62-1 0)

Checking the TGB for angular play ATA 64-20)

Main rotor blades leading edge and blade tip fairing check

ATA 62-1 0)

X-Ray inspection of MGB suspension bars ATA 63-32)

Ventilation flap control tangential bar

ATA

76-20)

Mechanical release control unit (Sling installation)

ATA

25-81)

Engine-to-MGB 23000 rpm input coupling

ATA

63-28)

Check and replacement of engine fire extinguishers

ATA

26-21)

Tail

boom - Check of the skin at frame 9000 or 9900 ATA

53-1 0)

Heater mat wiring modification

ATA

30-20)

Addition of a calendar time limit for the dynamic assemblies which are

maintained: - According to On-Condition procedures. - According to

their TBO

ATA

60-00)

Main Rotor Servo-control Attachment Bolts

ATA

67-30)

TIME LIMITS - MAINTENANCE CHECKS - Addition of a periodic check

of the engine fuel flow control

ATA

76-00)

LANDING GEAR - Check of the landing gear hydraulic unit ATA 32-30)

TIME LIMITS - MAINTENANCE CHECKS - Side plug doors ATA 52-11)

EQUIPMENT AND FURNISHINGS - Check

of

the inflation control system

of the optional life-raft installation ATA 25-69)

ICE AND RAIN PROTECTION - Heater mat wiring modification

ATA

30-20)

NAVIGATION - Maintenance

of

radar antenna slaving units

ATA

34-42)

TIME LIMITS - MAINTENANCE CHECKS - Emergency floatation gear:

Untimely deployment

ATA

25-62)

TIME LIMITS - MAINTENANCE CHECKS - Alternator bearings

ATA

24-20)

MAIN ROTOR DRIVE - Rotor brake control lever improved rotor brake

control lever operation corresponds

to MOD

0726696 ATA 63-23)

TAIL ROTOR - Maintenance applicable

to

the TRH pitch control

rod

bearing

in

the event of a hydraulic fluid leak

ATA

64-20)

TIME LIMITS - MAINTENANCE CHECKS - ICE AND RAIN

PROTECTION - De-icing system slip-ring

ATA

30-60).

TIME LIMITS - MAINTENANCE CHECKS - Changes

to

the maintenance

intervals of transformer-rectifiers MP/N 684-1009-200 ATA 24-30 and

ATA 25-64).


12/38

~ 3 9 C O P T E R

M INTEN NCE PROGR M

INTRODUCTION

1 GENERAL

1 1 Scope of the Maintenance

Program

The Maintenance Program

(PRE) is

drawn

up by

the aircraft manufacturer

and

it gives

all

the

maintenance operations that are to

be

performed by the operator.

It

specifies the mandatory limitations

and

operations to ensure that the aircraft airworthiness

is

maintained,

as

well

as

all the

operations

and

intervals, recommended

by the

manufacturer

and designed

to

ensure the operational availability of the aircraft, irrespective of its varied

operating missions.

1 2 Classification of the information

The

intervals specified

in

this

PRE

are

classified according

to

their importance into three

categories coded with stars (*):

**

Intervals

are

considered

to

be

mandatory. They

are

specified

in

the

Airworthiness

Limitations section.

No

margins

are

permissible.

Any changes to

an

interval can

be

negotiated only with the Manufacturer (EUROCOPTER)

and the EASA

(European Aviation Safety Agency).

*

Intervals beyond the margin

can be

adjusted subject

to

the approval

of

the Manufacturer

(EUROCOPTER)

and

supervisory authorities. The permissible margin complies with

Paragraph 2.5, unless

No

margin permissible

is

specified.

Intervals beyond the margin with

no

distinctive signs

can be

adjusted subject

to

the

approval

of the

Manufacturer (EUROCOPTER), providing compliance with the applicable

local authorities' regulations

is

ensured. The adjusted margin complies with Paragraph 2.5.

NOTE

The

*

or

**

classification can also be used

in

other manuals

(e.g. the

Maintenance Manual

(MET)).

In

this case,

it

applies

to

the procedure.

For example, a procedure

can

be classified **

with

an

interval not classified

**

.

1 3 Airworthiness Limitations

The airworthiness limitations are always subject

to

approval by the European Airworthiness

Authorities.


13/38

G ~ 3 9 C O P T E R

M INTEN NCE PROGR M

The operating time limits specified for the components guarantee flight safety with respect to

the

stress to which they are subjected. These limits

do

not constitute a commercial warranty.

It may be

necessary

to

remove

the

components before

the

listed time, based

on

other criteria

such as wear, fretting, corrosion ..

The only warranty applicable to the helicopter and to the components is that included in the

purchase agreement.

2 DEFINITIONS

2 1 Aircraft Maintenance

THE INITIAL

DATE

FOR AIRCRAFT AIRFRAME

AGING IS THE DATE THAT IS MARKED ON THE

IDENTIFICATION PLATE OF THE HELICOPTER

Maintenance covers

all the

operations intended to maintain

the

aircraft airworthiness, flight

readiness

and

performance in the course

of time.

It

includes monitoring, servicing

and the

repair of aircraft components

as

defined in

the

different

manuals, taking into account

all the

information that

the

aircraft manufacturer may need

to

pass

on

to

the operator Service Bulletins, Service

Telex,

Information

Telex,

Service Letters

... .

2 2 Types of

Maintenance

2 2 1

PREVENTIVE MAINTENANCE

Which

means all

scheduled, usually recurrent, actions

to

check

and

maintain a given

operational level.

2 2 2 CORRECTIVE MAINTENANCE

Which

means all the actions carried out further to a failure or a fault to restore the initial

operational level.

2 2 3 REMEDIAL MAINTENANCE

Which

means

all

the

actions designed

to

correct

an

anomaly and enable all or part of

the

preventive

and

corrective maintenance associated

with

this anomaly to

be

discontinued.

2 3 Maintenance Procedures

There

are

three

main

maintenance procedures:

- hard time maintenance,

-

on

condition maintenance,

- condition monitoring.


14/38

~ B C O P T E R

MAINTENANCE PROGRAM

defects that might affect the surface, the protection

and

paint coat of

the

components.

These defects must

be

examined

and

repaired immediately

in

compliance with the

applicable directives (criteria, then reconditioning).

Components and assemblies subject

to

OC maintenance are listed in Section

05.1 0.00.

The inspection intervals and the MET work cards

on

which the inspections are detailed,

are given

in

Section 05.20.01/02/03 of this

PRE.

The airworthiness inspection checks

are

marked

**

(two stars)

in

Section

05.20.01/02/03

and

called CHK

in

Section 05.99.00 of this

PRE.

2.3.3 Condit ion Monitoring

Remedial action

is

taken

on

a component subject

to

condition monitoring only after a

fault has been detected

on

it (without affecting flight safety).

The fault may be evidenced during a maintenance operation or

in

service. These

components are not therefore listed

in

a special chapter of this PRE.

2.4 Particular and Severe Operating Conditions

Certain climatic conditions are considered

to be

particular operating conditions.

They basically relate

to

operation:

-

in

damp tropical atmosphere

-

in

salt-laden atmosphrere

-

in

sand- and/or dust-laden atmosphere

-

in

cold weather

-

in

very cold weather

The limitations

and

maintenance procedures pertaining

to each

type of operating conditions

are covered with

all the

other tasks (refer

to

Sections 05.10.00

and

05.20.01 /02/03). The

particular operating condition

is

specified

in

the relevant task.

In these operating conditions,

in

addition to the routine maintenance operations, it is

necessary to apply the recommended preventive procedures

as

per Work Card 05.52.00.301.

As

no particular interval is specified, the operator will repeat these procedures according to

his own

experience gained

in

corresponding conditions.

2.4.1

Definitions:

Damp tropical atmosphere:

Helicopters operating

in the

following conditions: combinations

of high

temperatures

and

high humidity levels (from +

28

C

and 75 %

relative humidity).

Salt-laden atmosphere:

Helicopters operating

in the

following conditions:

- Helicopters based

on

a ship or based less than 1

km

inland for more than 50 of

the time,

or

- Flying offshore at low altitude (below 1 000 feet) for more than 5 of the time.


15/38

YJ39COPTER

M INTEN NCE PROGR M

2.5.1.2

2.5.1.3

Specific case:

Not applicable.

Intervals classified

as

1-star intervals

General

rule:

A margin

of 10%

limited:

-

to 300 H, for intervals expressed in flight hours,

-

to

6 months, for intervals expressed

in

calendar time,

- Not limited, for intervals expressed

in

a number

of

cycles or operations.

Important: This margin

of 10%

is

not

specified

in the

tasks concerned.

Specific case:

-

If

a specific margin

is

defined,

it is

specified

in the

task concerned.

-

If the

margin

is

equal

to

0, a no margin permissible annotation

is

specified

in

the task concerned.

Intervals classified

as

intervals with

no

star

General

rule:

A margin

of 10%

limited:

- to

300 H,

for intervals expressed

in

flight hours,

-

to

6 months, for intervals expressed

in

calendar time,

- Not limited, for intervals expressed in a number

of

cycles or operations.

Important: This margin

of

10% is

not

specified in the tasks concerned.

Specific case:

Not

applicable.


16/38

~ B C O P T E R

MAINTENANCE PROGR M

The

next application

of

this same maintenance operation A shall

be

carried out

at the

latest

at

X + Y i.e. 600 +

60

660 H.

In

all

cases, the interval between two maintenance operations shall not exceed the

maximum interval i.e. X +

Y

This principle is identical for intervals expressed

in

calendar time or cycles.

2 6 Authorization to install and transfer a component part or assembly) from one

aircraft version to another aircraft version

2 6 1

Components not Subject

to

In-Service Monitoring

2.6.2

2.6.2.1

2.6.2.2

2.6.2.3

2.6.2.4

Transfer of components not subject

to

in-service monitoring

is

authorized between any

versions;

in

particular, the mixability

of

such

components

is

thus authorized between civil

and

military versions.

Components Subject to In-Service Monitoring

Transfer Authorization

Transferring a component (part

or

assembly) listed

in the

PRE

from an

aircraft

version x to

an

aircraft version y

is

authorized only if the following conditions are

met

simultaneously:

- the aircraft versions x

and

y

are

those

in

the following list of SUPER

PUMA

versions:

AS

332

C,

332

C1,

332

L,

332 L

1,

332 L2 and

EC225.

The installation of components from any other aircraft version or type is prohibited,

- the part number of the component

to be

transferred

is

listed both

in

the

PRE of

version

x and

in

the

PRE

of version

y ,

-

no

temporary limitation for the component to be transferred is assigned in the

PRE

of version x or

in

the

PRE

of version

y ,

- it

is

prohibited

to

install version-specific

MOX

parts (parts resulting

from

a version

PUMA),

- it

is

prohibited

to

install version-specific

KUH [P]

or GTV parts.

Components Subject

to

a Service

Life

Limit

(SLL)

The transfer rules are defined

in

AIRWORTHINESS LIMITATIONS Section 05-99-00

of

this

PRE.

Components Subject

to an

Operating Time Limit (OTL)

Transfers

are

only authorized when the OTL limits are

the

same

and

final for each

of the versions.

The flight hours, cycles or calendar time

to be

logged

on

the new

version must

be

added to the flight hours already logged.

Components Subject to a Time Between Overhauls (TBO)

Transfers

are

only authorized when the TBO limits are

the

same

and

final for

each of the versions.


17/38

GLOSS RY

ABBREVIATIONS USED

A Basic inspection with a calendar interval

ALF:

ALL MP/N:

BFF:

C

CHK:

CSS:

CT:

D

E

EXC:

FC

G:

H

HT

INF:

M

MCM:

MEM:

MET:

MP/N:

NO

NOT

OC:

OpC:

OPT:

OTL:

S

SLL:

S/N:

T

TA

TBO

TSI

TSM

U

Y

:

:

Check After the Last Flight of the day

All part numbers

Check Before the First Flight

of

the day

Major inspection with a calendar interval

Airworthiness inspections

Chapter/Section/Subject

Work Card

Day

Maintenance due time

Except, except for

Functional Check

Major inspection with

an

interval

in

hours

Hour

Hard Time

Infinite service life

Month

Component Maintenance Manual

Engine Maintenance Manual

Maintenance Manual

Manufacturer's Part Number

Not Described

Non destructive Testing

On Condition Maintenance

Operational Check

Optional

Operating Time Limit

Supplementary inspection

Service Life Limit

Serial Number

Basic inspection with

an

interval

in

hours

Turn around check

Time Between Overhauls

Time Since Installation

Time Since Manufacture

Operating cycle

Year

Or - (See Section HOW TO USE THE PRE )

And

M INTEN NCE PROGR M


18/38

M INTEN NCE PROGR M

HOW T USE THE PRE

GENERAL LAYOUT

The Maintenance Program PRE) is made

up

of the following sections:

05 1

0-00 Intervals

This section lists the components subject to an Operating Time Limit OTL) or to a

limited Time Between Overhauls TBO) together with their corresponding intervals.

This section also lists the assemblies subject to On-Condition maintenance OC).

05-20-00 Maintenance Operations

This section lists the maintenance operations and their intervals

in

all the aircraft

operating conditions. It includes three sub-sections:

- 05-20-01 scheduled maintenance operations classified by Chapter/Section),

- 05-20-02 scheduled maintenance operations classified by intervals),

- 05-20-03 unscheduled maintenance operations classified by Chapter/Section).

For maintenance operations to

be

performed after incidents or during storage, refer to

the Maintenance Manual MET Chapter 05) or the Storage Manual MST) respectively.

Refer to the Engine Handbook for maintenance operations to be performed on the

power plant.

05-50-00 Special Monitoring

This section groups all the maintenance actions that are to be taken subsequent to

certain incidents or anomalies.

05-99-00 Airworthiness Limitations

This section lists all the components subject to a mandatory airworthiness limit SLL or

CHK) which must be applied in addition to the indications given in the other sections of

this manual.

The aircraft maintenance is to be carried out using all this information making reference to the

Work Cards in the Maintenance Manuals specifying the operating procedures.

NOTE

When applicable, depending on its necessity, the

operational procedure may

be

classified according

to the star codes defined in the Introduction to this

section.

In

addition to the information contained in the PRE, the aircraft manufacturer may require

additional monitoring operations or the embodiment of modifications.


19/38

~ ~ o p t e r

M INTEN NCE

PROGRAM

The effectivity (helicopter type

and

version)

is

indicated on

the

TITLE page

and

repeated at the

bottom of each page of

the

PRE.

4 MODIFYING AND UPDATING THE PRE

Each time he receives a revision

from

the aircraft manufacturer, the operator must update his

documentation. To this end, he will use the LIST OF EFFECTIVE PAGES given in both the

MAINTENANCE PROGRAM and AIRWORTHINESS LIMITATIONS sections. The date indicated at

the bottom of each page in each section

must

correspond to that indicated in these lists.

There are different types of Revisions: the Temporary Revision (TR), the Normal Revision (NR)

and the Customer Complement (CC).

4 1

Temporary Revision TR): Printed on yellow paper

4.1.1 General

EUROCOPTER may need to change points they consider to

be

important

in

the manual

between two normal revisions,

and

they do this by issuing Temporary Revisions.

The Temporary Revision covers crucial information that must be passed on rapidly and

cannot wait until the next Normal Revision

NR).

Several TRs may be issued between

two NRs.

The new DUs, whether revised or deleted, are issued

in

full on yellow paper. Changes

are identified by thick vertical lines

in

the right margin. TRs are identified by the number

of the next NR followed by a letter taken in alphabetical order

and

by a date: e.g.: 003b

identifies the second

TR

of the NR 002.

4.1.2 Content and Application

The Temporary Revision

is

made

up

of a Highlights unit, a List of Effective Pages

LOEP-TR and one or more Document Units.

The Highlights unit lists the major points covered by the TR. This information is issued

for each new TR.

The LOEP-TR identifies the new DUs, those revised and those deleted by the Temporary

Revision. The date marked on the DU

is

that of the TR

by

which

it

was modified. This

list

is

to be inserted at the beginning of the corresponding manual and, when necessary,

it

supersedes that issued previously. This list must

be

kept until the next NR.

The new DUs, those revised and those deleted:

- the new DU on yellow paper is to be inserted directly in the manual,

-

the

revised DU on yellow paper entirely supersedes the related DU issued on white

paper. The

DU on

white paper

is

to

be

removed from the manual.

- the DU that

is

to

be

deleted by the

TR is

issued on a single yellow page marked

DELETED . This page supersedes all the white pages of the Document Unit in

question and the white pages are to be removed from the manual.


20/38

M INTEN NCE PROGR M

OPTION L EQUIPMENT

1 COMPATIBILITY INCOMPATIBILITY

A system designed for specific operational requirements may sometimes impede other functions.

This incompatibility may be encoutered at two different levels:

In operation. The operating incompatibility of optional equipment is specified

in

the Flight Manual.

On installation on the aircraft:

- either provision is ensured on the helicopter for two optional systems but they cannot be

installed at the same time: installation incompatibility.

- or two optional systems can

be

installed at the same time provided that at least one of the

systems is modified: compatibility subject to certain conditions.

The following table lists the approved optional equipment and specifies any incompatibility,

capabilities subject to conditions and indicates when consequences on the helicopter operation are

specified in a Flight Manual Supplement.

2 TABLE OF THE APPROVED OPTIONAL EQUIPMENT INSTALLATIONS

INSTALLATION

CONDITIONAL

ITEM

DESCRIPTION

INCOMPATIBILITY WITH

INSTALLATION


Pilot's and Copilot s

47

Comfortable Seats

4CC Ice Detector

5 6

5

LEIGH Ice Detector

4

6

6

ROSEMOUNT Ice Detector

5

4

9

Ice-Trap System

16

SFIM Three-Axis Coupler

18

Installation

18

SFIM Four-Axis Coupler

16

Installation

26

Emergency Flotation Gear

27, 28

31 (1)

with External Fuel Tanks

27

Emergency Flotation Gear

26, 45, 46

31

( 1)

without External Fuel Tanks

28

Life Rafts in Sponsons

26, 45, 46

31

Skis Installation

(2) 36, 37 (1)

32

Semi-Retractable Main

Landing Gear


21/38

M INTEN NCE PROGR M

INSTALLATION

CONDITIONAL

ITEM

DESCRIPTION


INSTALLATION


58 LOCATOR Searchlight

72

36, 37 1)

59

Incandescent Flares

60 Public Address System

36,

37

1)

61 600-Liter Cabin Fuel Tank 49, 54, 56, 57, 74, 75, 76,

39,

40,

41

(3)

77, 78

55, 76, 77

74, 75 (5)

62

Abseiling Installation

50, 53, 72, 73, 75, 81, 82

54 (6)

51, 57

70

Reinforced Soundproofing

71

71

De Luxe Reinforced 70

Soundproofing

72

LH

Stairway Door

58,

62, 79, 80

73

RH Two-Panel Hinged Door

55, 56, 62, 79, 80

74

24-Utility Seats Installation

49, 50, 53, 56,

57,

75, 76,

48, 54, 61

(5)

77, 78, 79, 80, 81, 82

75

18-Crashworthy Utility Seats

49, 50, 53, 56, 57, 74, 76,

48, 54, 61

(5)

Installation

77, 78, 79, 80, 81, 82

76-77

20 and 19 Comfortable Seats

49, 50,

53,

56, 57, 74, 75,

48, 54, 61

(4)

Installation

78,

80, 81

82

78

18-Comfortable Seats

+

Toilet

49,

50,

53,

56,

57, 74,

75, 48, 54,

61

(4)

Installation

76,

77, 81

82

79

Baggage Hold Compatible

57, 72, 73, 7

4,

75, 79, 81,

with 20-Seats Installation

82, 83

80 Baggage Hold Compatible with

57, 72, 73, 74, 75, 79, 81

18-Seats + Toilet Installation

82,

83

81 10-12 VIP Seat Installation

48, 49, 50, 53, 54, 55, 56,

57, 61 62, 74, 75,

76,

77,

78, 79, 82

83 Aft Stairway Door 57, 70, 80

Legend:

1 ): Compatibility not demonstrated.

2): Incompatible with the tie-down function

in

the main landing gear wheel hub.

3): Incompatible with pressure refueling system.

4)

Compatible after removal of the front or rear seats.

5) Compatible after removal of the front seats.

6)

Compatible after re-arranging the seats.


22/38


23/38

G

~ B C O P T E R

MAINTENANCE PROGR M

GENER L

1 INTRODUCTION

This section lists the components and assemblies subject to

an

operating time limit OTL) or a

limited time between overhauls TBO) together with the corresponding intervals.

This section also lists the assemblies that are subject

to on

condition maintenance OC). The

inspection intervals of these assemblies are specified

in

this

PRE in

section 05.20.01/02.

The components are presented according

to ATA

standard 100 breakdown.

2 INTERVALS

For each component mentioned

in

this Section, the interval limit applies

to

the part number(s)

listed

and to all

successive dash numbers.

The

operator must confirm the validity of the installation of dash numbers with the EUROCOPTER

Customer Service Technical Support Department.

For

particular operating conditions, refer

to

the information given

in

Section INTRODUCTION

paragraph 2.4.

2 1

Operating

Time

Limit OTL)

Refer to Section INTRODUCTION, of this

PRE

for the definition of the operating time limit.

It may

be

expressed

in

flight hours, as a calendar time limit or as a number of

cycles/utilizations.

When several limits are indicated, the component

in

question must

be

removed

at

the first

limit reached.

2 2

Time Between Overhauls TBO)

Refer

to

Section INTRODUCTION, of this

PRE

for

the

definition

of

time between overhauls.

It

may

be

expressed

in

flight hours,

as

a calendar time limit or

as

a number

of

cycles/utilizations.

When several limits

are

indicated, the component

in

question must

be

removed at the first

limit reached.

A TBO applies to all the components of the assembly indicated.

3 INITIAL DATE OF EQUIPMENT AGING

Generally, the date

to be

taken into account

is

the date of first installation or first depreservation

of

the

equipment. This date

is to be

recorded

on

the equipment

log card

(FME).

In

some cases, the date

to be

taken into account

is

the date since manufacture recorded

on

the

equipment

log

card FME). In this case, the statement time since manufacture is indicated

in

the

DESCRIPTION column

in

this

PRE

section.


24/38

M INTEN NCE

PROGR M

HOW TO USE THE T BLES

1 GENERAL PRESENTATION

Description, documentation

Part number

Limit

CL

The parts, assemblies and components with a utilization or

an

operating time limit are listed

in

these tables according to the Chapter-Section-Subject breakdown of the ATA Specification 100 in

accordance with which the aircraft technical publications are produced).

2 DESCRIPTION PUBLICATION

The components subject to a limitation (OC, TBO, OTL) are listed in this column.

3 PART NUMBER

3 1 General

This column gives the manufacturer s part number for the component

in

question.

When applicable, the IPC gives the correspondence between the manufacturer s part number

and the EUROCOPTER identification number (704A.

..

).

These part numbers are also those which are used in all the support publications (MMA, IPC,

SBT,

etc.) and those which

can

be allocated a suffix used for spares purposes to indicate the

installation of an optional equipment item or of a specific configuration.

Example

The limitation given for the part number 332A33-0001-04 is also effective for

the assembly 332A33-0001-04M1.

3 2 Presentation

Components with the same description but with different part numbers are identified in the

following way:

MAIN OIL PUMP

4

TL:

TYPE OF LIMIT

This column defines the type of limitation:

o

on condition maintenance

31-751

03-4034-5

7034-400

7034-500

7034-600

TBO

3000 H


25/38

G

YB COPTER

M INTEN NCE PROGR M

05 10 00 REPERTORY

Chap/Sect

Description

age

21 52 ........................ OPT

AIR CONDITIONING.................................................

1

21 53 ........................ OPT FREON POD MOUNTED AIR CONDITIONING................... 1

22 30

........................

MOVEMENT CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

23 52

........................

OPT UNIT CONTROL CENTRALIZED .

........ .......

... . . .. . . . ... . . ... 1

23 71 ........................ OPT COCKPIT VOICE RECORDER..................................... 1

24 20

........................

AC GENERATING SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

24 30

........................ DC

GENERATING SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

24 31 ........................ BATTERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

25 00

........................

EQUIPMENT

AND

FURNISHING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

25 1 0 ........................ COCKPIT... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

25 62 ........................ OPT EMERGENCY FLOATATION GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

25 64 ........................ OPT HOIST.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

25 66 ........................ OPT EMERGENCY LOCATOR TRANSMITTER........................ 1

25 69

........................

OPT LIFE RAFTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

25 81 ........................ OPT SLINGS AND ACCESSORIES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

26 13

........................

MGB FIRE DETECTION SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

26 21 ........................ ENGINE FIRE EXTINGUISHERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

26 22 ........................ CABIN FIRE EXTINGUISHERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

28 10

........................

STOR AGE..................................................................... 1

28 20 ........................ FUEL DISTRIBUTION SYSTEM ............................................ 1

28 41 ........................ FUEL FLOWMETER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

28 93

........................

OPT FUEL

ICE

TRAP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

29 10

........................

MAIN HYDRAULIC SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

29 20

........................

AUXILIARY HYDRAULIC SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

30 20 ........................

AIR

INTAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

30 42 ........................ WINDSHIELD WIPERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

30 60 ........................ OPT DE ICING SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

31 20 ........................ CHRONOGRAPH............................................................. 1

32 12 ........................ RETRACTABLE MAIN LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

32 22

........................

NOSE LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

32 40 ........................ WHEELS AND BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

32 91 ........................ OPT SKIS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

33 20 ........................ OPT PASSENGER COMPARTMENT LIGHTING . . . . . . . . . . . . . . . . . . . . . . . 1

33 43

........................

LANDING LIGHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

33 45

........................

OPT SEARCHLIGHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

34 42 ........................ RADAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

34 43 ........................ OPT NAVIGATION COMPUTER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

35 30 ........................ PROTECTION AGAINST SMOKE.......................................... 1

36 1 0 ........................ P2 SUPPLY SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

45 11 ........................ OPT HUMS/CVFDR........................................................ 1

47 50

........................

OPT FUR INSTALLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . 1

55 10 ........................ HORIZONTAL STABILIZER . .

...

. ..... ... . . . .

...

.. . ....... .. . . . .....

...

.

...

. 1

62 35

........................ MAIN

ROTOR HUB/SHAFT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

62 37 ........................ BLADE PITCH CHANGE

ROD

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

63 10

........................

ENGINE TO MGB

COUPLING..............................................

1

63 20 ........................ MAIN GEARBOX . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

63 21

........................ OIL FILTER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1


26/38

Description, document tion

21 52

OPT AIR CONDITIONING

21/52/00/201/000/000

REGULATION FILTER FILTER ELEMENT

M T 21 52 00 201

Regulation filter

2

08ZE4.

Fitted

to

the air-conditioning units 3502A03

and 3502A04.

No

margin permissible.

21/52100/402/000/000

TURBO FAN COOLING UNIT

M T

21 52 00 402

Part number

CN15-05UJ

3202A0101

3202A0201

320280101

320280201

MAINTENANCE PROGRAM

T

21 52

TL

Limit

CL

OTL

1200 H

T8

1200 H


27/38

~ o p t e r

MAINTENANCE PROGRAM

T

21 53

Description document tion Part number

Limit

21 53

OPT

FREON

POD MOUNTED

AIR CONDITIONING

21/53/00/401/000/005

R22/R134A COLD AIR UNIT

788AA01 0101

788A040101

oc


28/38

~ 1 9 C O P T E R

Description document tion

Part number

22 30

MOVEMENT CONTROL

22/30/00/000/000/000

AUTOPILOT HYDRAULIC UNIT DISTRffiUTOR

30245

30245-001

22/30/00/000/000/005

AUTOPILOT HYDRAULIC UNIT DISTRffiUTOR

A84122-1

010-60666

22130/00/000/000/020

AUTOPILOT HYDRAULIC

UNIT

TRIM ELECTROVALVE

30010

22/30/00/000/000/021

67-770-1

67-770-2

AUTOPILOT HYDRAULIC UNIT SERVODISTRIBUTOR

30550-401

30550-501

22/30/00/000/000/022

AUTOPILOT HYDRAULIC UNIT SERVODISTRIBUTOR

A21495

A84 2

A84121-1

M T

22 30 10 403

22/30/1 0/401/000/000

HYDRAULIC UNIT

FILTER

FILTER ELEMENT

CG0140093411

NOO

M T

22 30 10 401

This filter cannot

be

cleaned. It must be

replaced if clogging

is

detected.

MAINTENANCE PROGRAM

T 22 30

T imit

CL

TBO 6000 H

TBO 6000 H

II

15

Y

TBO 6000 H

TBO 6000 H

TBO 6000 H

II

15 Y

OTL

3000 H


29/38

MAINTENANCE PROGRAM


Part number TL

23-52

OPT

-

UNIT CONTROL

CENTR LIZED

23/52/00/000/000/000

ETC 40XXF INSTALLATION, GPS/PTTI INTERFACE

C RD

- BATTERY

MET 23 52 XX 401

itted to the interface card 222-7012-201.

The operating time limit must

not

exceed

the

life

limit since manufacture.

No margin permissible.

23/52/00/000/000/0 10

222-3025-905 OTL

ETC 40XXF INSTALLATION, GPS/PTTI INTERFACE C RD - BATTERY

MET 23 52 XX 401

itted to the interface card 222-7012-201.

Life

limit since manufacture.


222-3025-905 OTL

T

23-52

Limit

CL

1

y

5 y


30/38

~ ~ B f C O P T E R


Part number

23 71

OPT COCKPIT VOICE RECORDER

23 71 01 /40 1 000/005

COCKPIT VOICE RECORDER

M T 23 71 XX 401

93A1 00-31

93A100-80

MAINTENANCE PROGRAM

ATA

23 71

T Limit

CL

TBO

4000 H

I

I


31/38


32/38


24 30

DC

GENER TING SYSTEM

24/30/00/402/000/000

TRANSFORMER RECTIFIER

MAINTENANCE PROGRAM

ATA 24 30

Part number

T

imit

CL

684-1009-200

oc


33/38

~ ~ p t r

Description

document tion

24 31 B TTERY

24/31/00/000/000/010

4 AH BATTERY

24/31/00/000/000/21 0

STANDBY BATTERY

Part number

40208-1

40208-5

40408

EEOOOS 011

EEOOOS 0111

MAINTENANCE PROGRAM

ATA 24 31

TL Limit

CL

oc

oc


34/38

MAINTENANCE PROGR M

T 25 00

Description, documentation

Part number

imit

25 00 EQUIPMENT

ND

FURNISHING

25/00/00/000/000/000

BELT HARNESS STRAPS MEDICAL INSTALLATION STRAPS

Life limit since manufacture.

Pilot, copilot, passenger and operator seat

belt and harness straps - Medical installation

straps.

For seat belts

and

harnesses fitted with

buckles manufactured by ANJOU refer to the

AIRWORTHINESS LIMITATIONS chapter.

Margin: 6 months

ALL MP/N OTL

10 y

*


35/38


Part number

25-10

COCKPIT

25 1 0 00 000 000 01

0

PILOT S

AND

COPILOT S

SEAT SHOCK ABSORBERS


25/1 0/00/000/000/020

251 1 02900-01

251 1 02900-02

3RD CREW MEMBER S SEAT SHOCK ABSORBER

2510107900

2510107901


MAINTENANCE PROGRAM

ATA 25-10

TL Limit

CL

OTL

5

y

OTL

5 y


36/38

Description

document tion

Part number

25 62 PT EMERGENCY FLOTATION GEAR

25/62/00/401/000/000

FORWARD CYLINDER

M T

25 62 00 401

Return the equipment to an approved repair

station for overhaul and replacement of the

unequipped bottle.

Interval starting from the date of manufacture.


25/62/00/401/000/020

FT CYLINDER

M T

25 62 00 401

Return the equipment to an approved repair

station for overhaul and replacement of the

unequipped bottle.

Interval starting from the date of manufacture.


202458-0

202458-1

202458-2

202458-3

158562-0

158562-1

158562-2

158562-3

MAINTENANCE PROGRAM

TL

Limit

L

OTL

15

OTL

15


37/38


25 64 O PT HOIST

25 64 00 000 000 020

HYDRAULIC HOIST 50 M CABLE

M M 25 62 21

M M 25 64 96

Life limit since manufacture in the original

packaging.

Normal climatic conditions.


25 64 00 000 000 021


M M

25 62 21

MCM 25 64 96


packaging.

Tropical and damp atmosphere.


25 64 00 000 000 022


M M

25 62 21

MCM 25 64 96


packaging.

Salt atmosphere.


Part number

709070

709070-100

709070

709070-100

709070

709070-100

MAINTENANCE PROGRAM

T 25 64

TL

Limit

L

OT

9 y

OT

7 y

OT

7 y


38/38


25/64/00/000/000/027

HYDRAULIC HOIST

50

CABLE

MCM 25 62 21

MCM 25 64 96

The operating time limit must not exceed the

life limit since manufacture.

Salt-laden atmosphere.


25/64/00/000/000/028

HYDRAULIC HOIST

50

M CABLE

MCM 25 62 21

MCM 25 64 96

The operating time limit must not exceed the

life limit since manufacture.

Sand-laden atmosphere.


25/64/00/402/000/000

HYDRAULIC HOIST

50

M

M T 25 64 00 402

With hydraulic motor.


25/64/00/403/000/005

HYDRAULIC HOIST SQUIB

MET 25 64 00 403

Life limit since manufacture n the original

Part number

709070

709070-100

709070

709070-100

76360-100

76360-110-01

76360-200

76360-210-01

76363-200-A

20CF4D

MAINTENANCE PROGRAM

ATA

25 64

TL

imit

CL

OTL 2 Y

II 500 U

OTL 2 Y

II

500 U

TBO 4 Y

II 1000 U

OTL

5 y

halaman ganjil

Documents