mel j-31 ,32 rev 03 mmel rev 15

INTENTIONALLY LEFT BLANK

AIRCRAFT: BAE J31/J32 MMEL REV. No. 15 DATE: 03/01/2007

AEROLINEAS SOSA

MINIMUM EQUIPMENT LIST

ALS REV: 01 DATE: 29/08/2007 PAGINA:

I

TABLE OF CONTENTS

-- Table of Contents I, II -- Control Page III – VI -- Log of Revisions V - VI -- Highlights of Change VII, VIII -- Distributions XI, X -- Procedure for item differed report XI – XIV -- Guidelines for (O) & (M) Procedures XV – XXII -- Definitions XXIII – XXVI -- Preamble XXVII, XXVIII 21 Air Conditioning 21-1, 2, 3, 4 22 Auto Flight 22-1, 2 23 Communications 23-1 THRU 4 24 Electrical Power 24-1, 2 25 Equipment/Furnishings 25-1 THRU 6 26 Fire Protection 26-1, 2 27 Flight Controls 27-1, 2 28 Fuel 28-1, 2 29 Hydraulic Power 29-1, 2 30 Ice and Rain Protection 30-1, 2, 3, 4 31 Indicating/Recording Systems 31-1, 2 32 Landing Gear 32-1, 2 33 Lights 33-1, 2, 3, 4 34 Navigation 34-1 THRU 6 35 Oxygen 35-1, 2 38 Water/Waste 38-1, 2 52 Doors 52-1, 2 57 Wings 57-1, 2 61 Propellers 61-1, 2 73 Engine/Fuel Controls 73-1, 2 74 Ignition 74-1, 2 76 Engine Controls 76-1, 2 79 Engine Oil 79-1, 2 82 Water Injection 82-1, 2

Aprobado Por_______________________ U.E.V, D.G.A.C de Honduras Firma________________________ Fecha_________________________


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CONTROL PAGE CHAPTER SECTION PAGE REVISION CHAPTER SECTION PAGE REVISION

Cover Page - 03 Table of Contents I 01 21

4

03 II 01

AUTO FLIGHT

22 22

1 2

01 01 Control Page III 03

IV 03 COMMUNICATION

23 23 23 23

1 2 3 4

01 01 01 01

Log of Revisions V 03

VI 01 Highlights of VII 03

ELECTRICAL

24 1

01 Change VIII 01

24

2

01 Distribution IX 01

X 01 EQUIPMENT/

FURNISHINGS 25 25

1 2

01 01

Procedure for item XI 01 25 3 01 Deferred report XII 01 25 4 03 XIII 01 25 5 01 XIV 01

FIRE

25

26

6 1

01

01 Guidelines for (O) XV 01 PROTECTION 26 2 01 & (M) Procedures XVI 01 XVII 01 FLIGHT

CONTROL 27 27

1 2

03 01 XVIII 01

XIX 01 FUEL

28

1

01 XX 01

XXI 03 28 2 01 XXII 01 HYDRAULIC

POWER 29 29

1 2

01 01 Definitions XXIII 01

XXIV 01 ICE AND RAIN

30

1

01 XXV 01

XXVI 01 PROTECTION 30 30

2 3

01 01

Preamble XXVII 01 30 4 01 XXVIII 01 INDICATING/

RECORDING SYS 31 31

1 2

01 01 AIR 21 1 01

CONDITIONING 21 2 01 LANDING GEAR

32

1

01 (ATA 21) 21 3 01

32 2 01


03

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CONTROL PAGE

CHAPTER SECTION PAGE REVISION CHAPTER SECTION PAGE REVISION LIGHT 33 1 01 WATER 82 1 01 33 2 01 INJECTION 82 2 01 33 3 01 33 4 01

NAVIGATION 34 1 01 34 2 01 34 3 01 34 4 01 34 5 01 34 6 01 OXYGEN 35 1 01 35 2 01 WATER / WASTE 38 1 03 38 2 01 DOORS 52 1 01 52 2 01 WINGS 57 1 01 57 2 01 PROPELLERS 61 1 01 61 2 01 ENGINE FUEL & 73 1 01 CONTROL 73 2 01 IGNITION 74 1 03 74 2 03 ENGINE 76 1 01 CONTROL 76 2 01 ENGINE OIL 79 1 02 79 2 01


03

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LOG OF REVISIONS

REVISION No.

ISSUE DATE

INSERTION DATE

INSERTED BY

SIGN

01 29/08/2007 02 29/04/2009 03 08/12/11


03

08-DIC-11


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VII

LISTA DE EQUIPO MÍNIMO CAMBIOS RELEVANTES (HIGHLIGHTS)

DESCRIPCIÓN TITULO SECCIÓN PAGINAS

Se agregó procedimiento de mantenimiento para el ítem 38-2

GUIDELINES FOR (O) & (M) PROCEDURES

XXI

En ítem 21-18 se agregó nota de aplicabilidad.

AIR CONDITIONING 21 21-4


EQUIPMENT / FURNISHING

25 25-4


FLIGHT CONTROLS 27 27-1


WATER / WASTE 38 38-1


IGNITION 74 74-1, 2

08-DIC-11

03


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IX

DISTRIBUCIÓN Cada copia de esta lista de equipo mínimo tendrá un numero de control en la carátula, una lista será archivada en la oficina del Gerente de Mantenimiento de AEROLINEAS SOSA, conteniendo el número de la copia de la lista de equipo mínimo, el nombre de la persona asignada, entidad o departamento al que pertenece, la firma de la persona responsable y la fecha cuando lo recibió. Para las listas abordo, el Jefe de Pilotos será la persona asignada y responsable de distribuir una copia en cada aeronave. Objetivo: El objetivo de distribuir esta lista de equipo mínimo es para que el personal involucrado en el despacho de vuelo tenga un documento para uso y orientación de los procedimientos operacionales y de mantenimiento que ALS utiliza para diferir el equipo inoperativo. Suministración: Solamente el Gerente de Mantenimiento puede suministrar copias de esta lista de equipo mínimo. Responsabilidad: Es responsabilidad el Gerente de Mantenimiento distribuir esta lista de equipo mínimo al personal involucrado en el despacho y proveer a cada aeronave con la copia actualizada correspondiente por modelo de aeronave. Así también de mantener actualizada la lista de distribución. Accesibilidad: Una copia de esta lista de equipo mínimo es conservada en la biblioteca de la empresa disponible para todo el personal pertinente u otro relacionado con estos procedimientos. Actualización: El personal que posee asignada una copia de esta lista de equipo mínimo es responsable de insertar la(s) revisión(es) en la lista de equipo mínimo y de registrarla(s) en la pagina asignada para tal efecto. La lista a bordo de la aeronave será actualizada por el Jefe de Pilotos. Verificación: Es responsabilidad del personal de Control de Calidad verificar que las lista de equipo mínimo en uso y a bordo de las aeronaves estén actualizados, para tal efecto el personal de Control de Calidad efectuara verificaciones periódicas en el lugar de trabajo. NOTA: No está permitida la reproducción total o parcial de esta lista de equipo mínimo sin la autorización por escrito del Gerente de Mantenimiento.


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XI

PROCEDIMIENTO PARA INGRESAR A DIFERIDO El piloto anota las fallas o discrepancias durante el vuelo o también puede anotar una falla el personal de Mantenimiento o de Control de Calidad, en la casilla de reportes de la tripulación (discrepancias). El personal de Mantenimiento debe tomar la acción correctiva pero cuando un reporte no se puede corregir por gestiones de mantenimiento tales como: Falta de repuesto, falta de equipo, falta de tiempo para corregir la discrepancia o desperfecto, o no esta la aeronave en la base; se debe abrir un Reporte Diferido. Para ingresar a diferido un instrumento o equipo se deben de cumplir las siguientes condiciones:

• Exista un MEL para la aeronave debidamente aprobado con su documento, por la DGAC de Honduras.

• El MEL contemple las limitaciones del fabricante y la DGAC. • El MEL este provisto para la operación de esa aeronave con instrumentos y equipo inoperativo. • La bitácora posee una hoja para diferidos en la cual se anotan los instrumentos y equipos

inoperativos. • La aeronave debe de ser operada bajo las condiciones y limitaciones aplicables a la aeronave,

contenidas en el MEL. Personas autorizadas para utilizar el MEL: El personal que ingrese a diferido equipo o instrumentos es previamente autorizado por el Gerente de Mantenimiento o en su defecto por el Jefe de Control de Calidad. El personal de Mantenimiento puede utilizar el MEL sin necesidad de pedir una autorización adicional a la DGAC, siempre y cuando el MEL se use en conexión con las operaciones efectuadas con esa aeronave bajo las Regulaciones de Aviación civil de Honduras RAC OPS I Y II. Calificación del personal para ingresar a diferido: Licencia de mecánico emitida por la DGAC, Tipo I vigente. Habilitación en la categoría de la aeronave que está manteniendo, haber recibido instrucciones sobre el procedimiento de ingreso a diferidos y uso del MEL.


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PROCEDIMIENTO PARA INGRESAR A DIFERIDO Procedimiento: Se puede entrar a diferido el equipo o sistema siempre y cuando este contemplado en la lista de equipo mínimo conocida internacionalmente por sus siglas en ingles como MEL. Para ingresar un ítem a diferido se debe cumplir con el procedimiento siguiente:

1. Se consulta la lista de equipo mínimo de la aeronave, si es posible ingresarlo a diferido se deben

verificar las limitaciones ya sea de operación o de mantenimiento, (remarks.) 2. Se ingresa a diferido la discrepancia trasladando la falla textualmente como la describió el piloto a la

hoja de diferidos de la aeronave. 3. Se completa la bitácora anotando la respuesta de la discrepancia indicando que fue ingresada a diferido,

el número de la hoja de diferidos, la referencia del MEL y la categoría del diferido. 4. El personal de Mantenimiento toma todas las acciones pertinentes al diferido que sea requerido por el

MEL en la sección de observaciones como “O”, “M”, que indiquen, por ejemplo desconectar alguna conexión eléctrica, instalación de un collar en los rompe circuitos o instalación de dispositivos de bloqueo, etc.

5. El personal de Mantenimiento instalará un rótulo en el indicador o panel del sistema entrado a diferido

así como en el espacio correspondiente en la bitácora con la fecha de ingreso y la referencia del MEL. 6. Seguidamente se elabora una tarjeta de control de trabajo para la discrepancia entrada a diferido

anotando en la casilla de notas a la referencia del MEL. 7. Si el diferido está pendiente de corregir por falta de partes se debe elaborar una orden de compra y

anotar el número de esta en la hoja de diferidos y en la tarjeta de control de trabajo en su casilla correspondiente.

8. Al tener los datos de la bitácora completos se debe dar el retorno al servicio para que la aeronave

continué el vuelo, este retorno es responsabilidad del personal de Mantenimiento autorizado por ALS y Control de Calidad debe de verificar que todo está completo.

9. La aeronave operara el período que le permite la categoría del diferido como lo son Categoría A: Las

horas asignadas por el MEL, Categoría B: Tres días, Categoría C: Diez días y la Categoría D: 120 días. 10. El corregir la discrepancia y sacar la falla de diferido se debe de hacer en el periodo permitido por el MEL

lo cual es responsabilidad de Mantenimiento y Control de Calidad debe de verificar que no se excedan los limites y se corrija la falla adecuadamente como lo requieren el programa de mantenimiento, el manual de mantenimiento del fabricante y este manual.


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PROCEDIMIENTO PARA INGRESAR A DIFERIDO 11. Después de haber tomado las acciones correctivas, se remueven todos los rótulos y dispositivos

instalados durante el diferido, si el manual de mantenimiento requiere pruebas funcionales u operacionales se efectúan y se retorna a servicio la aeronave, todo lo anterior es efectuado por el personal de Mantenimiento en conjunto con el personal de Control de Calidad.

12. Al corregir la discrepancia en diferido se completa la tarjeta de control de trabajo, se hace una anotación

en la hoja de bitácora iniciando por abrir la orden de corrección en la casilla de reportes de la tripulación y cerrándola con la acción de mantenimiento en la casilla de acciones correctivas así mismo completando las casillas de la hoja de diferidos en la cual se anota que el diferido fue cerrado.

El personal de Control de Calidad es responsable por que se cumpla este procedimiento y de darle el seguimiento respectivo desde que se ingresa la falla a diferido, operación de la aeronave con el diferido, hasta la toma de acciones correctivas de los diferidos cerrados, así como de que los documentos tales como bitácora, hoja de diferidos, tarjeta de control de trabajo y órdenes de compra estén debidamente completados.

REPORTES DIFERIDOS FUERA DE LA BASE:

Cuando algún instrumento o equipo falle fuera de la base y este puede ser entrado a diferido de acuerdo al MEL.

El Capitán de la nave debe de contactarse con el departamento de Operaciones de ALS para que se le emita las instrucciones pertinentes. Lo único que el Capitán podrá efectuar fuera de la base y con instrucciones del departamento de Mantenimiento es instalar la calcomanía de INOP (Inoperativo) sobre el instrumento o equipo que esta fallido. Esta calcomanía debe completarse con los siguientes datos como lo son: Referencia del MEL y la Fecha de ingreso.

En la bitácora de la aeronave el Capitán debe de ingresar el reporte e indicar que coloco la calcomanía con instrucciones del departamento de Mantenimiento para que se corrija al llegar a la base y se cierre el reporte en la bitácora de acuerdo a los procedimientos del Manual de Procedimientos de Mantenimiento de ALS.

Cantidad de Reportes Diferidos

La cantidad total de reportes diferidos permitidos en el avión es de ocho, el numero de reportes diferidos permitidos por sistema (ATA) es de tres. Ambos casos son permitidos siempre y cuando los reportes diferidos no involucren unidades que estén interrelacionadas entre si de acuerdo a su operación y restricción del MEL.


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21-1 (M) Maintenance procedure to ensure that no electrical or mechanical fault exists which

would have an adverse effect on any other System. a. Verify the opposite side air-conditioning group provides adequate heating and cooling

by operating only the appropriate side engine and monitoring the air ducts verifying an adequate conditioned air supply is present.

b. Position inoperative air-conditioning selector valve to OFF position. c. Pull and secure appropriate temperature control circuit breaker,

21-2 (M) Maintenance procedure to ensure the failed Valve is in the CLOSED/OFF position.

a. Verify the operable Flow Control Valve provides adequate heating, cooling and pressurization by operating only the appropriate side engine and monitoring the air ducts verifying an adequate conditioned air supply is present.

b. Verify the failed Flow Control Valve is in the CLOSED position by operating only the appropriate sides engine and monitoring the air ducts, No airflow should be present with the Flow Selector in the OFF position

c. Position inoperative air-conditioning selector valve to OFF position. 21-11 (M) Maintenance procedure to ensure the Discharge Valve or Safety Valve is secured OPEN.

Secure the Discharge Valve located on the forward face of the rear pressure bulkhead OR the Safety Valve located on the left hand aft face of the forward pressure bulkhead lo the full OPEN position may be accomplished with the use of a wooden dowell or similar instrument secured across the opening with safety wire or tywraps.

21-13 (M) Maintenance procedure to ensure no electrical or mechanical fault exists.

a. Insure no rnechanical fault exists with the Freon air conditioning system that may affect the operation of other aircraft's systems located in the vicinity of the failed system.

b. Pull and secure the air conditioning blower circuit breaker. c. Pull and secure the air conditioning controller circuit breaker. NOTE: Deactivation of the A/C Controller Circuit Breaker disables the Aux Heater

System. 21-14 (M) Maintenance procedure to ensure the Discharge Valve or Safety Valve is secured OPEN.

Secure the Discharge Valve located on the forward face of the rear pressure bulkhead to the full OPEN position. Securing the valve to the full OPEN position may be accomplished with the use of a wooden dowell or similar instrument secured across the opening with safety wire or tywraps.


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XVI

GUIDELINES FOR (O) & (M) PROCEDURES 21-15 (M) Maintenance procedure to ensure the Discharge Valve or Safety Valve is secured OPEN.

Secure the Safety Valve located on the left hand aft face of the forward pressure bulkhead to the full OPEN position. Securing the valve to the full OPEN position may be accomplished with the use of a wooden dowell or similar instrument secured across the opening with safety wire or tywraps.

21-18 (M) Maintenance procedure to inspect Ground Heater to ensure no electrical or mechanical

fault exists which would have an adverse effect on any other System.

a. Visually inspect the affected heater Insuring no mechanical fault exists that would have an adverse effect on any other aircraft system located in the vicinity of the failed system.

b. Pull and secure appropriate circuit breaker when applicable. c. Remove power fuse when applicable.

21-19 (M) Maintenance procedure to inspect Main Wheel Bay to ensure Air Conditioning Duct

System integrity.

a. Position inoperative air-conditioning selector to the OFF position. b. Verify the opposite side air conditioning group provide adequate heating and cooling

by operating only the appropriate side engine and monitoring the air ducts verifying an adequate supply of conditioned air is present.

c. Visually inspect the affected air conditioning duct system located in the main wheel bay area for security and signs of bleed air leaks that may have affected other components within the leak area.

d. In the event bleed air leaks exist, repairs to damaged areas or components are to be made prior to scheduled service flight.

21-20 (M) Maintenance procedure to ensure no electrical or mechanical fault exists which could

have an adverse effect on any Flight Control function.

a. Position inoperative air conditioning system to the OFF position. b. Verify the opposite side air conditioning group provides adequate heating and cooling

by operating only the appropriate side engine and monitoring the air ducts verifying an adequate supply of conditioned air is present.

c. Visually inspect the affected air conditioning duct area located in the vicinity of the Overheat Temperature Switch and Water Separator for security and signs of bleed air leaks that may have affected other components within the leak area.

d. In the event bleed air leaks exist, repairs to damaged areas or components are to be made prior to scheduled service flight.


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GUIDELINES FOR (O) & (M) PROCEDURES 22-1 (M) This item do not apply in AEROLINEAS SOSA fleet. 22-2 (M) This item do not apply in AEROLINEAS SOSA fleet. 22-3 (M) Maintenance procedure to ensure no electrical or mechanical fault exists which could

have an adverse effect on any Flight Control function.

a. Pull and secure appropriate circuit breaker. b. Visually inspect Yaw Damper Servo and Control Cable to rudder insuring no

obstructions exist. c. Disconnect and secure electrical connections to Yaw Damper Servo. d. Operate rudder once the above a, b, c procedures have been accomplished insuring

free movement of the rudder exists. 23-2-1 (O) Operations procedure to ensure appropriate briefings are provided to the passengers.

(Applies to both provisos.)

The .non-flying. pilot will give appropriate oral briefings directly to the passengers. These briefings will include pre-takeoff pre-landing, after-landing, and any additional briefings required as deemed necessary by the flight crew.

23-3 (O) Operations procedure to ensure appropriate briefings are provided to the passengers.

The .non-flying. pilot will give appropriate oral briefings directly to the passengers. These briefings will include pre-takeoff pre-landing, after-landing, and any additional briefings required as deemed necessary by the flight crew.

23-9 (O) This item do not apply in AEROLINEAS SOSA fleet. 23-9-1 (O) This item do not apply in AEROLINEAS SOSA fleet. 23-11 (O) This item do not apply in AEROLINEAS SOSA fleet. 23-12 (O) This item do not apply in AEROLINEAS SOSA fleet. 23-14 (O) This item do not apply in AEROLINEAS SOSA fleet. 24-4 (O) Operations procedure to ensure both Inverters are operative.

Flight crew must verify operation of both inverters by ensuring the normal/transfer switch is in the normal position and all associated RED captions are not illuminated


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GUIDELINES FOR (O) & (M) PROCEDURES 25-2-2 (O) Operations procedure to alert Cabin Crew of inoperative Restraining Bar.

The flight crew will alert the passenger of the seat behind the inoperative bar stows his/hers belongings in a most immediate and convenient place.

25-8-2 (M) This item do not apply in AEROLINEAS SOSA fleet. 25-8-2 (M) This item do not apply in AEROLINEAS SOSA fleet. 25-10 (M) This item do not apply in AEROLINEAS SOSA fleet. 25-15-1 (O) This item do not apply in AEROLINEAS SOSA fleet. 25-15-2 (O) This item do not apply in AEROLINEAS SOSA fleet. 25-15-3 (O) This item do not apply in AEROLINEAS SOSA fleet. 25-16 (M) Maintenance procedure to ensure Seat is locked in the appropriate position.

a. Seat to be adjusted to pilots requested position, insuring with the crew, full flight control movement and normal visibility is available.

b. Lock seat into position once the above Paragraph .a. is accomplished. c. Visually verify locking plunger is engaged prior to accomplishing Para. d. d. Seat adjustment mechanism to be disconnected and stowed to prevent interference

with other systems or components. 25-18 (M) This item do not apply in AEROLINEAS SOSA fleet. 25-19 (M) This item do not apply in AEROLINEAS SOSA fleet. 25-21 (M) Maintenance procedure to ensure cargo loading limits from an approved source are

observed.

See Weight and balance report and AOM section 7 26-5 (M) This item do not apply in AEROLINEAS SOSA fleet. 26-6 (M) This item do not apply in AEROLINEAS SOSA fleet. 27-4 (M) Maintenance procedure to ensure Flight Control functions are not adversely affected.

a. Verify that all flight controls are functional and unimpaired while the controls are moved through the full range of travel.

b. Visually verify that ALL flight control (aileron, rudder and elevator) lock pins are fully retracted and the bias springs retain the plungers in the UNLOCKED position.


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GUIDELINES FOR (O) & (M) PROCEDURES 27-5 (M) This item do not apply in AEROLINEAS SOSA fleet. 28-1 (O) Operations procedure to determine fuel on board meets regulatory requirements for the

intended flight. Crew will determine fuel quantity prior to each flight by use of the drip less sticks. 30-9-3 (O) Operations procedure to ensure a satisfactory field of vision is available to the crew. Using the three position switch, turn the system ON and OFF until a satisfactory parked

position is achieved. 30-14 (O) Operations procedure to verify the Engine Anti-Ice System is operative.

Run the speed levers up. Open the engine anti-ice valve on the affected engine on the EGT gauge. An increase indicates the system is operating properly.

31-2 (O) This item do not apply in AEROLINEAS SOSA fleet. 32-2 (M) Maintenance procedure to verify the Normal Brake Accumulator is checked.

a. Verify both Foot Brake Applied Pressure Gauges are operative. b. Visually verify Normal Brake Accumulator is showing correct charge.

33-2-1 (M) Maintenance procedure to deactivate the Fluorescent Lighting System and ensure specific

follow-up action is performed in accordance with the applicable AD.

Turn the Fluorescent Lighting System OFF and install placard by the switch reading .DO NOT OPERATE. NOTE: This is an approved alternate means of compliance. Reference Aerospace Lighting Corporation A.D. 90-14-06 which is superseded by A.D. 95-22-01.

33-3 (O) Operations procedure to ensure ground deicing procedures do not require the use of

Wing Illumination Lights. No icing condition is present during ground operation. 34-17 (O) Operations procedure to ensure Autopilot with Altitude Hold is operative and enroute

operations do not require use of the Altitude Alerting System. Autopilot not installed in AEROLINEAS SOSA fleet. 34-20 (O) Operations procedures to determine, prior to departure, items required in the provisos

operate normally and Positive Radar Control can be maintained by ATC on the enroute portion of the flight. (Applies to all provisos.)

a. Set and compare Gyros.


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GUIDELINES FOR (O) & (M) PROCEDURES 34-21 (M) Maintenance procedure to ensure TCAS Unit is deactivated and secured. (Applies to both

provisos.)

Pull and secure appropriate circuit breaker. 34-22 (M) Maintenance procedure to ensure TCAS Unit is deactivated and secured. (Applies to both

provisos.)

Pull and secure appropriate circuit breaker. 34-22-2 (M) This item do not apply in AEROLINEAS SOSA fleet. 34-22-3 (M) This item do not apply in AEROLINEAS SOSA fleet. 34-23 (O) Operations procedure to establish and ensure use of alternate procedures.

Monitor the altimeters closely. 34-23-(a) (O) Operations procedure to establish and ensure use of alternate procedures.

Monitor the altimeters closely.

34-23-(d) (O) Operations procedure to establish and ensure use of alternate procedures. (Applies to both provisos.) Monitor the altimeters closely.

34-23-(e) (O) Operations procedure to establish and ensure use of alternate procedures. (Applies to both provisos.) Monitor the altimeters closely.

34-23A-2 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-23B-1 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-23B-1(a) (O) This item do not apply in AEROLINEAS SOSA fleet. 34-23B-1(d) (O) This item do not apply in AEROLINEAS SOSA fleet. 34-23B-1(e) (O) This item do not apply in AEROLINEAS SOSA fleet. 34-23C-1 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-25 (O) This item do not apply in AEROLINEAS SOSA fleet.


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XXI

GUIDELINES FOR (O) & (M) PROCEDURES 34-26 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-27 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-28 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-29-1 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-30-1 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-32 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-33 (O) This item do not apply in AEROLINEAS SOSA fleet. 34-34 (O) This item do not apply in AEROLINEAS SOSA fleet. 35-3 (M) Maintenance procedure to ensure Flight Deck Gauge is operative. This procedure should

also ensure the person charging the Oxygen System is continuously aware of the pressure reading of the Flight Deck Gauge.

a. Verify Flight Deck Gauge is operative b. Recharging of the system must be accomplished with an individual located in the Flight

Deck monitoring the Flight Deck Gauge and in full communication with the individual servicing the system.

CAUTION: Service system at a slow rate to avoid overheating of service ports and lines. 38-1 (M) This item do not apply in AEROLINEAS SOSA fleet. 38-2 (M) Maintenance procedure to ensure components are deactivated or isolated and System

has no leaks. (M) Maintenance procedure to ensure components are deactivated or isolated, the Pilot-In-

Command determines the flight duration is acceptable with Lavatory unusable and the Door is secured CLOSED and placarded.

52-1 (O) Operations procedure for flight crew members to confirm by visual inspection that the

Door is latched prior to departure. A flight crew member must confirm by visual inspection that the door is latched prior to

departure. 52-4 (M) Maintenance procedure to secure Cargo Bay Door.

a. Ensure Aft Cargo Bay is empty of all baggage. b. Close Aft Cargo Bay door and secure the Security Shoot Bolts in the locked position. c. Securing of the Security Shoot Bolts to accomplished utilizing safety wire.


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52-6 (O) Operations procedure to ensure the Door is supported externally and only one

passenger is on the Door at a time.

The flight crew will have the door opened and closed by the station personnel. A crew member will be present at the door whenever passengers are boarding or departing the aircraft to ensure only one person uses the stairs at a time.

74-2 (O) Operations procedure to ensure Continuous Ignition is operative.

Before each flight, the Pilots are to operate the ignition system for each engine before start and listen for the igniters Snapping.

79-1 (O) Operations procedure to verify proper Oil Cooler Flap operation prior to departure. Proper operation will be confirmed by the First Officer while the Captain operates the

switches. 79-3 (M) Maintenance procedure to deactivate the System.

a. Verify opposite side Oil Cooler Flap operates normally. b. Verify affected Oil Cooler Flap is in the CLOSED position. c. Disconnect and secure electrical connection from affected Oil Cooler Flap.

(O) Operations procedure to ensure AFM limitations and performance are complied with.

Pilots are to observe POH performance limitations. Oil pressure and temperature limitations are to be monitored in accordance with POH limitations.

(M) Maintenance procedure to deactivate the System.

a. Verify opposite side Oil Cooler Flap operates normally. b. Verify affected Oil Cooler Flap is in the OPEN position. c. Disconnect and secure electrical connection from affected Oil Cooler Flap.

(O) Operations procedure to ensure AFM limitations are complied with.

Pilots are not to exceed 150 KIAS maximum for flight. Oil pressure and temperature limitations are to be monitored in accordance with POH limitations.


AEROLINEAS SOSA



XXIII

DEFINITIONS

1. System Definitions. System numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are numbered sequentially. a. "Item" (Column 1) means the equipment, system, component, or function listed in the "Item" column. b. "Number Installed" (Column 2) is the number (quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., passenger cabin items) a number is not required. c. "Number Required for Dispatch" (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met. NOTE: Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Administrator. d. "Remarks or Exceptions" (Column 4) in this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes. e. A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text for the current revision of that page only. The change bar is dropped at the next revision of that page. 2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type certification and approved by the responsible FAA Aircraft Certification Office. The FAA approved AFM/RFM for the specific aircraft is listed on the applicable Type Certificate Data Sheet. 3. "As required by FAR" means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Federal Aviation Regulations operating rules. The number of items required by the FAR must be operative. When the listed item is not required by FAR it may be inoperative for the time specified by repair category. The term “14 CFR” may be substituted for “FAR” in MMELs or operator MELs. 4. Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment condition. NOTE: To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified, placard wording and location will be determined by the operator.


AEROLINEAS SOSA



XXIV

DEFINITIONS 5."-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed. 6. "Deleted" in the remarks column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft. 7."ER" refers to extended range operations of a two-engine airplane (ETOPS) which has a type design approval for ER operations (ETOPS) and complies with the provisions of Advisory Circular 120-42A. 8. "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal Aviation Act and Federal Aviation Regulations. 9. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or local time, as established by the operator, during which at least one flight is initiated for the affected aircraft. 10. "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft (structural) or in the engine(s) (induction). 11. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for operation with the listed item inoperative. 12. ”Inoperative" means a system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or tolerance(s). 13. ”Notes:" in Column 4 provides additional information for crewmember or maintenance consideration. Notes are used to identify applicable material which is intended to assist with compliance, but do not relieve the operator of the responsibility for compliance with all applicable requirements. Notes are not a part of the provisos. 14. Inoperative components of an inoperative system: Inoperative items which are components of a system which is inoperative are usually considered components directly associated with and having no other function than to support that system. (Warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MMEL). 15. "(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative. Normally these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as part of the operator's manual or MEL.


AEROLINEAS SOSA



XXV

DEFINITIONS 16. "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by the flight crew however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as a part of the operator's manual or MEL. NOTE: The (M) and (O) symbols are required in the operator's MEL unless otherwise authorized by the Administrator. 17. "Deactivated" and "Secured" means that the specified component must be put into an acceptable condition for safe flight. An acceptable method of securing or deactivating will be established by the operator. 18. "Visual Flight Rules" (VFR) is as defined in FAR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan. 19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under Instrument Flight Rules. 20. "Visible Moisture" means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow. 21. "Passenger Convenience Items" means those items related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ash trays, stereo equipment, overhead reading lamps, etc. 22. Repair Intervals: All users of an MEL approved under FAR 121, 125, 129 and 135 must effect repairs of inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators: Category A. Items in this category shall be repaired within the time interval specified in the remarks column of the operator's approved MEL. Category B. Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and 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 malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.


AEROLINEAS SOSA



XXVI

DEFINITIONS Category D. Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days (2880 hours), excluding the day the malfunction was recorded in the aircraft maintenance log and/or record. 27. "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft maintenance log and or record. This day is excluded from the calendar days or flight days specified in the MEL for the repair of an inoperative item of equipment. This provision is applicable to all MEL items, i.e., categories "A, B, C, and D." 28. “Considered Inoperative”, as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item shall not be used or operated until the original deferred item is repaired. Additional actions include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MEL provisions, including any (M) and (O) procedures and observing the repair category. 29. “Is not used” in the provisos, remarks or exceptions for an MEL item may specify that another item relieved in the MEL “is not used.” In such cases, crewmembers should not activate, actuate, or otherwise utilize that component or system under normal operations. It is not necessary for the operators to accomplish the (M) procedures associated with the item. However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used to inform crewmembers that a component or system is not to be used under normal operations. 30. Nonessential equipment and furnishings (NEF) are those items installed on the aircraft 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’s 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. NEF items are not items already identified in the MEL or CDL of the applicable aircraft. They do not include items that are functionally required to meet the certification rule or for compliance with any operational rule. Operator’s NEF process shall not provide for deferral of items within serviceable limits identified in the manufacturer’s maintenance manual or operator’s approved maintenance program such as wear limits, fuel/hydraulic leak rates, oil consumption, etc. Cosmetic items that are fully serviceable but worn or soiled may be deferred under an operator’s NEF process.


AEROLINEAS SOSA



XXVII

PREAMBLE

The following is applicable for AEROLINEAS SOSA operating under RAC OPS I: The DGAC Regulations require that all the equipment installed on the aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not be necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not necessary when the remaining operative equipment can provide an acceptable level of safety. A Master Minimum Equipment List (MMEL), is developed by State Aviation Inspection, with participation by the aviation industry, to improve aircraft utilization and thereby provide and thereby provide more convenient and economic air transportation for the public. The approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the DGAC finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations: it does not contain obviously required items such as wings, flaps, and rudders. The MMEL is the basis for development of ALS’S MELS which take into consideration the ALS’S particular aircraft equipment configurations and operational conditions. ALS’S MEL’S for DGAC, may include items not contained in the MMEL; however, relief for administrative control items must be approved by the DGAC. An ALS’S MEL, may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual ALS’S MEL, when approved and authorized, permits operations of the aircraft with inoperative equipment. Equipment not required by the operation being conducted and equipment in excess of RAC requirements are include in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative. Suitable conditions and limitation in the from of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained. The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability the MMEL establishes limitation on the duration of conditions for operation with inoperative equipment. The MEL provides for release of the aircraft for flight with inoperative equipment.


AEROLINEAS SOSA



XXVIII

PREAMBLE When an item of equipment is discovered to be inoperative, it is reported by marking and entry in the aircraft Maintenance Record/Logbook as prescribe by DGAC regulations. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to DGAC prior to further operations. MEL condition and limitation, do not relieve ALS from determining that the aircraft is in condition for safe operation with items of equipment inoperative. When this requirements are meet, and Airworthiness Release, Aircraft Maintenance Record/Logbook entry, of other approved documentation is used as prescribed by DGAC Regulations. Such documentation is required Prior to operation with an item of equipment inoperative. ALS is responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on the aircraft operation and crew workload will be considered. ALS established a procedure in General Maintenance Manual that include the parts, personnel, facilities, procedures, and schedules to ensure timely repair. WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.


AEROLINEAS SOSA


ALS REV: 01 DATE: 15/06/2003 PAGINA: 21-

1

SYSTEM & SEQUENCE NUMBERS

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3 NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING 4. REMARKS OR EXCEPTIONS

1. Air Conditioning Group C 2 1 (M) One may be inoperative provided the opposite side System provides adequate heating and cooling.

2. Flow Control Valves C 2 1 (M) One may be inoperative provided:

a) Components of the opposite side System provide adequate heating, cooling and pressurization,

b) Failed Valve is in CLOSED/OFF position and

c) Cabin Altitude Warning Caption is operative.

3. Temperature Controllers

(Automatic and Manual) C 4 2 May be inoperative provided one

Temperature Controller (Automatic or Manual) is operative on each side.

4. Recirculation Fan C 1 0 May be inoperative

5. Cabin Differential Pressure Indicator

C 1 0 May be inoperative for unpressurized flight.

C 1 0 May be inoperative for pressurized flight

provided: a) Cabin Altitude Indicator is operative, b) Cabin Altitude Warning System is

operative and c) A Cabin Altitude Conversion Chart

is available to the Cockpit Crew in flight. (Located in Emergency Checklist section).


AEROLINEAS SOSA



2


1. REPAIR CATEGORY

2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING 4. REMARKS AND EXCEPTIONS

6. Cabin Altitude Indicator C 1 0 May be inoperative for unpressurized flight. C 1 0 May be inoperative for pressurized flight

provided: a) Cabin Differential Pressure Indicator

is operative, b) Cabin Altitude Warning System is

operative and c) A Cabin Altitude Conversion Chart

is available to the Cockpit Crew in flight. (Located in Emergency Checklist section).

7. Cabin Altitude Warning

Caption C 1 0 May be inoperative for unpressurized flight.


provided: a) Aircraft is operated at or below

10,000 feet MSL, b) Cabin Differential Pressure Indicator

is operative and c) Cabin Altitude Indicator is operative.

8. Cabin Pressure/Rate of

Change Indicator C 1 0 May be inoperative for unpressurized flight.


provided all other Pressurization Indicating and Warning Systems are operative.


AEROLINEAS SOSA



3


1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING 4. REMARKS AND EXCEPTIONS

9. Pressurization Controller (Automatic Function)

C 1 0 May be inoperative for unpressurized flight provided the Discharge Valve or Safety Valve is OPEN.


provided: a) Pressurization can be adjusted

using the Manual System and b) All other Pressurization Indicating

and Warning Systems are operative.

10. Manual Pressurization

Control (Rotating Knob) C 1 0 May be inoperative for unpressurized flight.


provided: a) Automatic function of the

Pressurization Controller is operative and

b) All other Pressurization Indicating and Warning Systems are operative.

11. Pressurization Dump

Control (Toggle Switch) C 1 0 (M) May be inoperative for unpressurized

flight provided the Discharge Valve or Safety Valve is secured OPEN.

12. Absolute Air Pressure

Regulator C 1 0 May be inoperative for unpressurized flight.

13.

Freon Air Conditioner System

D 1 0 (M) May be inoperative.

14. Discharge Valve C 1 0 (M) May be inoperative for unpressurized

flight provided the Discharge Valve or Safety Valve is secured OPEN.


AEROLINEAS SOSA


ALS REV: 03 DATE: 08-DIC-11/2003 PAGINA: 21-

4


1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

21 AIR CONDITIONING

15. Safety Valve C 1 0 (M) May be inoperative for unpressurized flight provided the Discharge Valve or Safety Valve is secured OPEN.

16. Cabin Punka Louvres DELETED REVISION 12.

17. Cabin Temperature Indicator

C 1 0 May be inoperative

18

Cabin Ground Heater D 1 0 (M) May be inoperative. (J31 only, J32 unistalled)

19. Over Temperature Caption (Main Wheel Bay)

C 2 1 (M) One may be inoperative provided: a) Associated Air Conditioning Group is

selected OFF and b) Opposite side provides adequate

heating and cooling.

20. Duct Over Temp Caption (O/TEMP)

C 2 1 (M) One may be inoperative provided: a) Associated Air Conditioning Group is

selected OFF and b) Opposite side provides adequate

heating and cooling.


AEROLINEAS SOSA


ALS REV: 01 DATE: 29/08/2007 PAGE: 22-

1


1. REPAIR CATEGORY

2. NUMBER INSTALLED


4. REMARKS AND EXCEPTIONS

22 AUTO FLIGHT 1. Autopilot B 0 0 Not installed on Aircraft.

Is mandatory two crew members pilots For flight in IFR operations. RAC OPS 1 1.655

2.

Yaw Damper (As a Component of Autopilot)

This item N/A by autopilot not installed.

3.

Yaw Damper (Not a Component of Autopilot)

C 1 0 (M) Maybe inoperative provided flight controls are not adversely affected.

4. Autopilot Disconnect

Functions (Quick Release Controls)

This item N/A by autopilot not installed.


AEROLINEAS SOSA


ALS REV: 01 DATE: 29/08/2007 PAGE: 22-

2



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1


1. REPAIR CATEGORY

2. NUMBER INSTALLED


4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS 1. Communications Systems

(VHF and UHF) D 2 0 Any in excess of those required by RAC OPS

I may be inoperative provided the flight Is conducted under VFR on routes navigated by visual reference and provided it is no powered by the emergency AC bus, emergency DC transfer bus and not required for emergency procedures.

1) VHF Communications Control Panels

a) Frequency Transfer Light C 2 0 May be inoperative

b) Frequency Transfer Switch C 2 0 May be inoperative

c) Frequency Selector Knob C 4 2 Two may be inoperative provided the fault is not located on the same transceiver.

d) Frequency Indication C 4 2 Two may be inoperative provided the fault is

not located on the same transceiver.

2. Passenger Address System (PA)

1) Passenger Configuration B 1 0 (O) May be inoperative provided:

a) Alternate, normal and emergency procedures, and/or operating restrictions are established and used.

NOTE: Any Station function(s) that operate normally may be used.

(continued)


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ALS REV: 01 DATE: 29/08/2007 PAGE: 23-

2


1. REPAIR CATEGORY

2. NUMBER INSTALLED


4. REMARKS OR EXCEPTIONS

23 COMMUNICATIONS

2. Passenger Address System (PA) (Continued)

1) Passenger Configuration (Continued)

C

1 0 (O) May be inoperative provided: a) PA not required by RAC OPS 1.695

and b) Alternate, normal and emergency

procedures, and/or operating restrictions are established and used.

NOTE: Any station function(s) that operate normally may be used.

2) Cargo Configuration D

1

0

May be inoperative provided procedures do not require its use.

3.

Recorded Passenger Address System

D 1 0 (O) May be inoperative

4. Static Discharge Wicks C 12 7 No more than one Discharge Wick may be missing from:

a) Left Wing, including Aileron, b) Right Wing, including Aileron and c) Each Empennage Control Surface.

5. Cockpit Speakers System D 2 0 May be inoperative provided two operative Headsets are available to the flight crew.

6. Audio Amplifiers DELETED REVISION 10.


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3


1. REPAIR CATEGORY

2. NUMBER INSTALLED


23 COMMUNICATIONS 4. REMARKS OR EXCEPTIONS

7. Cockpit Voice Recorder

(CVR) 1 1 Must be operative IAW RAC OPS 1 1.700)

8. Boom Microphones A 2 0 May be inoperative provided repairs are made

within three flight days.

9. Selective Call Systems (SELCAL)

D 0 0 Not installed on Aircrafts

10.

Touchtone Microphones (DTMF)


11.

ACARS System D 0 0 Not installed on Aircrafts

12.

ACARS Printer D 0 0 Not installed on Aircrafts

13. Electronic Checklists D 0 0 Not installed on Aircrafts

14. High Frequency (HF) Communication System


15. Emergency Locator Transmitter (ELT)

1 1 Must be operative IAW RAC OPS 1.1820


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ALS REV: 01 DATE: 29/08/2007 PAGE: 23-

4



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ALS REV: 01 DATE: 29/08/2007 PAGE: 24-

1


1. REPAIR CATEGORY

2. NUMBER INSTALLED


24 ELECTRICAL POWER 4. REMARKS OR EXCEPTIONS

1. Ammeters B 2 1 One may be inoperative provided the corresponding Generator (GEN) Fail Caption is operative.

2. Inverters DELETED BY MMEL REVISION 9

3. Generator (GEN) Fail Captions

B 2 1 One may be inoperative provided Ammeter corresponding to the inoperative Generator (GEN) Fail Caption is operative and monitored.

4. Red Inverter (INV) Failure Caption

B 1 0 (O) May be inoperative

5. External Power Receptacle C 1 0 May be inoperative

6. Voltmeter Function Selector Switch

1) Main Bus Position C 1 0 May be inoperative provided Battery Bus Position is operative.

2) Ground Power Position C 1 0 May be inoperative provided Battery Bus Position is operative.


AEROLINEAS SOSA


ALS REV: 01 DATE: 29/08/2007 PAGE: 24-

2



AEROLINEAS SOSA


ALS REV: 01 DATE: 29/08/2007 PAGE: 25-

1


1. REPAIR CATEGORY

2. NUMBER INSTALLED

3.

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/ FURNISHINGS


1. Cockpit Crewmember Shoulder Harness

DELETED BY MMEL REVISION 10.

2. Passengers Seat(s) C 19 0 May be inoperative provided: a) Seat does not block an Emergency

Exit, b) Seat does not restrict any

passenger from access to the main aircraft Aisle and

c) The affected Seat(s) are blocked and placarded “DO NOT OCCUPY”.

NOTE 1: A Seat with an inoperative Seat Belt is considered inoperative.

NOTE 2: Affected Seat(s) may include the Seat(s) behind and/or adjacent outboard Seats.

1) Recline Mechanism

C 0 0 Not installed on Seats

(continued)


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ALS REV: 01 DATE: 29/08/2007 PAGE: 25-

2


1. REPAIR CATEGORY

2. NUMBER INSTALLED

3.




2. Passenger Seats (Continued)

2) Under seat Baggage Restraining Bars

C 19 0 (O) May be inoperative provided: a) Baggage is not stowed under Seat

with inoperative Restraining Bar, b) Associated Seat is placarded “DO

NOT STOW BAGGAGE UNDER THIS SEAT” and

c) Procedures are established to alert Cabin Crew of inoperative Restraining Bar.

3) Armrest C 19 0 May be inoperative or missing and Seat occupied provided:

a) Armrest does not block an Emergency Exit,

b) Armrest does not restrict any passenger from access to the main aircraft Aisle and

3.

Seat Tray DELETED BY MMEL REVISION 10. NOTE: Seat Tray is considered a Passenger Convenience Item.

4. Cockpit Folding Door/Curtain

C 1 0 May be inoperative provided Door/Curtain is secured OPEN and does not block egress to exit.


AEROLINEAS SOSA


ALS REV: 01 DATE: 29/08/2007 PAGE: 25-

3


1. REPAIR CATEGORY

2. NUMBER INSTALLED

3.




5. Passenger Convenience/ NEF Items

1)

Passenger Convenience Items

Passenger convenience items, as expressed in this MEL are those related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ashtrays, stereo equipment, overhead reading lamps. Items addressed elsewhere in this document shall not be included.

a)Overhead Reading Lamps D 19 0 May be inoperative

b) Cabin Punka Louvers

D 21 0 May be inoperative

2)

Non-Essential Equipment & Furnishings (NEF)

- 0 May be inoperative, damaged, or missing provided that the item(s) is deferred in accordance with the AEROLINEAS SOSA guidelines. (M) and (O) procedures, if required, must be available to the flight crew.


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ALS REV: 03 DATE: 08-DIC-11 PAGE: 25-

4


1. REPAIR CATEGORY

2. NUMBER INSTALLED




6. Emergency Locator Transmitter

RELOCATED TO ITEM 23-15, REVISION 15 OF MMEL.

7. Observer Seat(s)

1) Primary Observer Seat (Including Associated Equipment)

A 0 0 Not installed on Aircrafts Note: A passenger seat in the pass cabin is available to an DGAC inspector for the performance of official duties.

8. Flight Attendant Seats 0 0 Not installed on Aircrafts

9. Pilot and Co-pilot Armrest C 4 0 May be inoperative provided armrest is secured in the UPRIGHT position.

10. Lavatory 0 0 Not installed on Aircraft J31, see ATA 38 for J32

11.

Flotation equipment D 21 0 Aircraft must be equipped with a life vest or flotation cushion for each occupant if the aircraft is operated over water and beyond power off gliding distance to shore or for extended over water operation.

12. Ground Heater Moved to ATA 21

13. Sun visors C 2 0 May be inoperative provided there are no visual restrictions to the flight crew.

14. Cargo Net (Carry on Baggage Area)

C 1 0 May be inoperative provided the carry on baggage area is empty.


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5


1. REPAIR CATEGORY

2. NUMBER INSTALLED

3.




15. Emergency Medical

Equipment

First Aid Kit (FAK) 1 1 Must be operative according to RAC OPS 1

1630 and 1745.

16. Crew Seat Adjustment A 4 0 (M) May be inoperative provided:

a) Seat(s) are locked in a position that permits normal pilot visibility,

b) Full Flight Control movement is available,

c) Position of Seat is acceptable to the crew and

d) Repairs are made within one flight day.

17. Exterior Lavatory Door Ashtrays

- - - Not installed on Aircrafts

18. Galley Waste Receptacles

Access Doors/Covers - - - Not installed on Aircrafts

19. Overhead Storage Bin(s)/Cabin and Galley Storage Compartment/ Closets


20. “FASTEN SEAT BELT WHILE SEATED” Sign or Placard

C 1 0 Placard may be illegible or missing provided a legible Sign or Placard is visible from each occupied Passenger Seat.


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6


1. REPAIR CATEGORY

2. NUMBER INSTALLED

3.




21. Cargo Restraint Systems C 1 0 (M) May be inoperative or missing.


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ALS REV: 01 DATE: 29/08/2007 PAGE: 26-

1


1. REPAIR CATEGORY

2. NUMBER INSTALLED

3.


26 FIRE PROTECTION 4. REMARKS OR EXCEPTIONS

1. Portable Fire Extinguisher(s)

2 2 Both must be operatives according to RAC OPS 1 1.790

2.

Pod Smoke Detector C 1 0 May be inoperative NOTE: Pod Smoke Detector relief and “C” repair interval are not applicable if Detector is disconnected or removed in accordance with FAA Approved Service Bulletin.

3. Fire Bottle Discharge Discs C 4 0 May be missing provided the Bottle Pressure is verified prior to each departure.

4. Cargo Compartment Fire Detection/Suppression Systems

C 1 0 May be inoperative provided associated Cargo Compartment remains empty. NOTE 1: Does not preclude the carriage

of empty cargo containers, pallets, ballast, etc.

NOTE 2: Class E Cargo Compartments

require only the installation of Smoke or Fire Detection Systems (not suppression).

5.

6.

Lavatory Fire Extinguisher System Lavatory Smoke Detection System

- -

- -

- -

Not installed on Aircrafts Not installed on Aircrafts


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ALS REV: 01 DATE: 29/08/2007 PAGE: 26-

2



AEROLINEAS SOSA

MINIMUN EQUIPMENT LIST


1


1. REPAIR CATEGORY

2. NUMBER INSTALLED

3.


27 FLIGHT CONTROLS 4. REMARKS OR EXCEPTIONS

1. Trim Tab Position Indicators (Ailerons)

C 1 0 May be inoperative provided: a) Tab is visually checked for full range of

operation, b) Tab operation is not impaired and c) Tab is positioned to NEUTRAL prior to

each departure and NEUTRAL is verified by visual inspection.

2. Trim Tab Position Indicators (Rudder)

C 1 0 May be inoperative provided: a) Tab is visually checked for full range of

operation, b) Tab operation is not impaired and c) Tab is positioned to NEUTRAL prior to

each departure and NEUTRAL is verified by visual inspection.

Applicable only for J31

3. Flap Position Indicator C 1 0 May be inoperative provided: a) External Flap Position Markings are

present on the left and right Flap Vanes,

b) Flaps are visually checked for full travel and Flap operation is not impaired and

c) Flaps are visually checked for proper setting prior to each departure.

4. Control Lock System C 1 0 (M) May be inoperative provided all Flight Control Functions are not impaired. NOTE: Limited to 20 kts tailwind

5.

Electric Elevator Trim

C

1

0

Not installed on Aircrafts

6. Flap Lift Dump System C 1 0 May be inoperative provided performance charts which provide data for landing distances without Lift Dump are used.


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28 FUEL 4. REMARKS OR EXCEPTIONS

1. Fuel Quantity Gauges C 2 1 (O) One may be inoperative provided: a) A reliable means is established to

determine that fuel on board meets the regulatory requirements for the intended flight and

b) Both Fuel Flow Meters are operative and monitored.

2.

Fuel Counter/Consumed Indicator


3. Fuel Cross-Feed Light C 1 0 May be inoperative provided: a) Proper operation of Cross-Feed System

is checked prior to departure, b) Both Fuel Pressure Annunciator Lights

are operative and c) Both Fuel Quantity Gauges are

operative.

4.

Low Level Fuel Warning Lights

C 2 0 May be inoperative provided associated Fuel Quantity Gauge is operative.

5.

Magnetic Fuel Level Indicators

C 8 0 May be inoperative provided: a) A reliable means is established to

determine that fuel on board meets the regulatory requirements for the intended flight and

b) Both Fuel Flow Meters are operative.

6.

Fuel Boost Pump

A

2

1

One may be inoperative provided:

a) Opposite Pump is operative, b) Fuel Cross-Feed is operative, c) Flight is conducted at or below Flight

Level 200, d) Jet A or Jet A-1 fuel is used and e) Repairs are made within three flight

days.


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29 HYDRAULIC POWER 4. REMARKS OR EXCEPTIONS

1. Hydraulic Pump Pressure Gauges

C 2 1 One may be inoperative provided: a) Both Pumps are confirmed operative

each time Engines are started and b) Hydraulic System High Pressure

Warning Caption is operative.

2. Hydraulic System High Pressure Warning Caption (HYD)

C 1 0 May be inoperative provided Hydraulic Pump Pressure Gauges are operative and monitored.


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30 ICE AND RAIN PROTECTION


1. Surface Deicing System (Wing, Vertical and Horizontal Stabilizer)

C 1 0 May be inoperative provided aircraft is not operated in known or forecast icing conditions.

2. Surface De-Ice System (Automatic Function Only)

C 1 0 May be inoperative provided Manual Control is operative.

3. Airfoil De-Ice Pressure Indication Lights


4. Windscreen Heating System C 2 0 May be inoperative provided aircraft is not operated in known or forecast icing conditions.

5. Windscreen Demisting System

C 1 0 May be inoperative provided both Windscreen Heaters are operative.

6. Windshield Magnetic Heating Indicators


7. Pitot Heaters (No.1 and No.2)

B 2 0 Left Unit must be operative for IFR passenger carrying and/or for flight in known or forecast icing conditions. Two heated Pitot Tubes are required for these conditions if a second Airspeed Indicator is installed and operative.

8. Pitot Heater (No. 3) B 1 0 May be inoperative provided Flight Director is not used.


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9. Windshield Wipers C 2 0 May be inoperative provided aircraft is not operated in precipitation within 5 nautical miles of the airport of takeoff or intended landing. RAC OPS 1 1.645.

1) Slow Speed C 1 0 May be inoperative provided high speed is operative.

2) High Speed C 1 0 May be inoperative provided: a) Slow speed is operative and b) Slow speed is adequate to remove

water from the Windshield.

3) Park Mode C 2 0 (O) May be inoperative provided the Wiper Blade is manually parked in a position providing a field of vision satisfactory to the flight crew.

10. Stall Vane and Pitot Heater Indicating Lights

B 3 0 May be inoperative provided aircraft is not operated in known or forecast icing conditions.

11. Stall Warning Vane Heaters C 2 0 May be inoperative provided aircraft is not operated in known or forecast icing conditions.

12.

Elevator Horn Anti-Icing System

C 1 0 May be inoperative provided Autopilot is not operated during flight into known or forecast icing conditions.

13. Propeller De-Icing System (Includes Ammeters)



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14. Engine Anti-Ice Indicators C 2 1 (O) One may be inoperative provided: a) An operational check is performed

before each flight and b) Aircraft is not operated in known or

forecast icing conditions.

15. Engine Inlet Anti-Icing Systems

C 2 1 One may be inoperative provided aircraft is not operated in visible moisture and OAT is less than +5 degrees Centigrade.


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31 INDICATING/ RECORDING SYSTEMS


1. Clocks With Sweep Second Hand or Electric Digital Clocks.

C 2 0 May be inoperative for VFR flight.

C 2 1 One may be inoperative for IFR flight.

2.

Flight Hour Recorder C 0 0 Not installed on Aircrafts

3.

Flight Data Recorder (FDR) System

A 0 0 Not installed on Aircrafts Note: CVR must be operative IAW RAC OPS 1 1.700


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32 LANDING GEAR 4. REMARKS OR EXCEPTIONS

1. Foot-Brake Applied Pressure Gauges

C 2 0 May be inoperative provided: a) All other Brake System Gauges are

operative and b) Brakes are checked for proper

operation prior to departure.

2. Main Brake Supply Pressure Gauge

C 1 0 (M) May be inoperative provided: a) Both Foot Brake Applied Pressure

Gauges are operative and b) The normal Brake Accumulator is

showing the correct charge.


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33 LIGHTS 4. REMARKS OR EXCEPTIONS

1. Cockpit/Flight Deck/Flight Compartment and Instrument Lighting System

C 6 3 Individual lights may be inoperative provided remaining Lights are:

a) Sufficient to clearly illuminate all required instruments, controls, and other devices for which it is provided,

b) Positioned so that direct rays are shielded from flight crewmembers eyes and

c) Lighting configuration and intensity is acceptable to the flight crew.

2. Cabin Lights

1) Aircraft Equipped With ALC Lighting System

(HR-ATA)

A 1 0 Individual Lights may be inoperative provided: a) Lighting configuration at the time of

departure is acceptable to the flight crew and

b) Repairs are made within 5 flights or 10 flight hours whichever occurs first.

OR

C 1 0 (M) May be inoperative.

2) All Other Aircraft (HR-ATE)

C 1 0 Individual Lights may be inoperative provided lighting configuration at the time of departure is acceptable to the flight crew.

3. Wing Illumination Lights C

2

0

(O) May be inoperative provided ground de-icing procedures do not require their use.


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4. “No Smoking/Fasten Seat Belt” Sign

C 1 0 May be inoperative provided appropriate verbal briefings are given to passengers.

5. Position Light(s) C 3 0 May be inoperative for day operations.

C 3 3 May be inoperative for night operations provided at least one Bulb is operative in each position (i.e., left Wing Tip, right Wing Tip, and Tail).

6. Upper Beacon Light C 1 0 May be inoperative for day operations.

C 1 0 May be inoperative for night operations provided Wing Tip Strobe Light System is operative.

7. Lower Beacon Light C 1 0 May be inoperative for day operations.

C 1 0 May be inoperative for night operations provided Wing Tip Strobe Light System is operative.

8. Wing Tip Strobe Light System

C 1 0 May be inoperative for day operations.

C 1 0 May be inoperative for night operations provided both Upper and Lower Beacon Lights are operative.


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9. Landing Lights C 2 0 May be inoperative for day operations.

C 2 1 One may be inoperative for night operations.

10. Taxi Light C 1 0 May be inoperative for day operations.

C 1 0 May be inoperative for night operations provided both Landing Lights are operative.

11.

Logo Light System D 1 0

12. Spar Caution Light (With or Without Flasher)

C 1 0 May be inoperative provided passengers are appropriately briefed regarding Spar Step.

13, Baggage Compartment Light


14.

Pod Baggage Compartment Light



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15.

Recognition Light System C 1 0 May be inoperative

16.

Window Wash Lights C 15 0 May be inoperative.

17.

Exterior Light Pulsing Systems

a) Landing Light Pulse System


b) Navigation Light Pulse System


c) Logo Light Pulse System D 0 0 Not installed on Aircrafts


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34 NAVIGATION 4. REMARKS OR EXCEPTIONS

1. Gyroscopic Rate of Turn

Slip/Skid Indicators B

B

2

2

0

1

May be inoperative for day VFR flights. One must be inoperative for IFR and night VFR flights IAW RAC OPS 1 1.652.

2. Vertical Speed Indicator B

B

2

2

0

1

May be inoperative for day VFR flights. One must be operative for IFR and night VFR flights IAW RAC OPS 1 1.652.

3. ATC Transponders and

Automatic Altitude Reporting Systems

D

2

1

One must be operative IAW RAC OPS 1 1.860 and 1.865

1) Elementary and

Enhanced Downlink Aircraft Reportable Parameters


4.

Long Range Navigation Systems

C

0

0

Equipment not installed.

5. Navigation Equipment

a) VOR Receivers C 2 1 One may be inoperative as long as the flight is not conducted under IFR or VFR over routes not navigated by visual reference over the terrain, RAC OPS 1 1.865.


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b) ILS Systems

1) Glideslope Receiver C 2 0 May be inoperative provided approach does not require its use.

2) Localizer Receiver C 2 0 May be inoperative provided approach does not require its use.

6.

Global Positioning System (GPS)

D 1 0 May be inoperative provided enroute navigation and approach procedures are not dependent on its use.

7. Weather Radar/Thunderstorm Detection Equipment Systems

C 1 0 May be inoperative provided: Aircraft may not dispatched into known thunderstorm activity, RAC OPS 1 1.670.

8. Radar Stabilization C 1 0 May be inoperative

9. Marker Beacon C 2 0 May be inoperative provided approach does not require its use.

10.

Flight Director C 1 0 May be inoperative provided landing minimums are not based on its use.

11.

Radar Altimeter C 1 0 May be inoperative provided landing minimums are not based on its use.

NOTE 1: GPWS may be affected.

12. Altitude Encoder Combined with ATA 34-3.


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13. Distance Measuring Equipment (DME) Systems

D

1 1

1 0

Must be operative IAW RAC OPS 1 1865 May be inoperative for VFR over routes navigated by visual reference over the terrain, RAC OPS 1 1.860

14.

Standby Attitude Indicator C

1 1

1 0

Must be operative IAW RAC OPS 1 1865 May be inoperative for VFR over routes navigated by visual reference over the terrain, RAC OPS 1 1.860

15. Automatic Direction Finding Systems (ADF)

C

1 1

1 0

Must be operative IAW RAC OPS 1 1.865 May be inoperative for VFR over routes navigated by visual reference over the terrain, RAC OPS 1 1.860

16. RMI (Radio Magnetic Indicators)

C 2 0 May be inoperative.

17. Altitude Alerting System C 1 0 May be inoperative. RAC OPS 1 1.660

18.

Page Reader C 0 0 Not installed on Aircrafts

19.

Externally Mounted Airspeed/Altimeter Bugs

C 4 0 May be inoperative, broken or missing provided there are no internal connections.


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20. Non-Stabilized Magnetic Compass

B 1 0 (O) May be inoperative provided any combination of three Gyro or INS (IRU) Stabilized Compass Systems are operative.

B 1 0 (O) May be inoperative provided: a) Any combination of two Gyro or INS

(IRU) Stabilized Compass Systems operate normally and

b) Airplane is operated with Dual Independent Navigation Capability and under Positive Radar Control by ATC on the enroute portion of the flight.

B 1 0 (O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are installed, operate normally, and used in conjunction with approved Free Gyro Navigation Techniques.

RAC OPS 1 1.650

21. Traffic Alert Collision Avoidance System (TCAS I)

C 1 0 (M) May be inoperative provided: a) Not required by RAC, b) System is deactivated and secured and c) Enroute or approach procedures do not

require its use

22. Traffic Alert and Collision Avoidance System (TCAS II)

0 0 Not required in this aircraft IAW RAC OPS 1 1.668.


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23. Ground Proximity Warning System (GPWS)

A 1 0 (O) May be inoperative provided: a) Alternate procedures are established

and used and b) Repairs are made within two flight

days.

a) Modes 1-4 A 1 0 (O) May be inoperative provided: a) Alternate procedures are

established and used and b) Repairs are made within two flight

days.

b) Test Mode A 1 0 May be inoperative provided: a) GPWS is considered inoperative and b) Repairs are made within two flight

days.

c) Glideslope Deviation(s) (Mode 5)

C 2 1 One may be inoperative

d) Advisory Callouts B 2 0 (O) May be inoperative provided alternate procedures are established and used.

C

2

0

(O) May be inoperative provide:

a) Advisory callout not require by RAC and b) Alternate procedures are established

and used.

24.

Flight Profile Advisory System

D 0 0 Not installed on aircrafts

25.

Wind Shear Warning and Flight Guidance System (Reactive)

- - Not installed on aircrafts

26.

Wind Shear Detection and Avoidance System (Predictive)

- - Not installed on aircrafts


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27. Wind shear Warning and Flight Guidance System (Reactive)

0 0 Not installed on aircrafts

28. Wind shear Detection and Avoidance System (Predictive)

0 0 Not installed on aircrafts

29. Flight Management System 0 0 Not installed on aircrafts

30. Navigation Management System

Not installed on aircrafts

31. Automatic Dependent Surveillance-Broadcast (ADS-B) System


32. Multifunction Display (MFD) Not installed on aircrafts

33. Multifunction Display (MFD) Cooling Fan


34. GPS Switching Unit Base - - Not installed on aircrafts


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35 OXYGEN 4. REMARKS OR EXCEPTIONS

1. Oxygen System (Passenger)

C 1 0 May be inoperative provided: The time flown at cabin pressure of 10,000 feet is not more than 30 min.

C 19 0 Individual Masks, Dispensers or associated Doors may be inoperative provided the affected Seat(s) is blocked and placarded “DO NOT OCCUPY”.

2. Oxygen Pressure Gauge (Passenger Bottle)

C 1 0 May be inoperative provided Flight Deck Gauge is operative.

3. Oxygen Pressure Gauge (Charging)

C 1 0 (M) May be inoperative provided Flight Deck Gauge is operative.

4. Oxygen Pressure Gauge (Flight Deck)

C 1 0 May be inoperative provided: a) Charging Gauge is operative and b) Aircraft is operated at or below

10,000 feet MSL.

5. Bay Temperature Gauge D 1 0 May be inoperative provided: a) Bay temperature is determined prior

to servicing and b) A calibrated thermometer is used to

determine temperature.

6. Protective Breathing Equipment (PBE)

2 2 Must be operative IAW RAC OPS 1 1.780


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38 WATER/WASTE 4. REMARKS OR EXCEPTIONS

1. Potable Water Systems - - Not installed on Aircrafts

2. Lavatory Waste Systems - - (M) Individual Components may be inoperative provided:

a) Associated Components are deactivated or isolated and

b) Associated System Components are verified not to have leaks

c) Lavatory drawer is locked and placared INOPERATIVE – DO NOT USE.

NOTE: Any portion of a System which operates normally may be used.

Applicable only on J32


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52 DOORS 4. REMARKS OR EXCEPTIONS

1. Pod Door Caption C 1 0 (O) May be inoperative

2. Entry Door Caption (Not Illuminated)

A 1 0 May be inoperative provided: a) Fasten Seat Belt Sign is operative

and illuminated throughout the flight,

b) Flight is conducted using minimum necessary Cabin Differential Pressure,

c) Door is visually verified CLOSED and LOCKED per AFM procedures prior to each departure and

d) Repairs are made within two flight days.

NOTE: If Entry Door Caption is illuminated,

follow AFM procedures.

3. Pod Door Restraint Cable C 1 0 May be inoperative

4. Aft Cargo Bay Door Latches C 2 0 (M) May be inoperative provided Cargo Bay is empty and secured CLOSED.

5. Passenger Door Seal C 1 0 May be inoperative provided: a) Flight is conducted in an

unpressurized configuration and b) Dump Valve is selected OPEN.

6. Cabin Door Restraint Cable C 1 0 (O) May be inoperative provided: a) Door is supported externally when

OPENED and CLOSED, b) Only one passenger at a time is

allowed to be on the Door and c) Handrail/Door Stay is fully

serviceable.


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57 WINGS 4. REMARKS OR EXCEPTIONS

1. Vortex Generators A 20 16 One or two may be missing from each Wing provided:

a) They are not adjacent, b) They are not located on Wing Root

Fillets, c) Wing Surface and Wing Root Fillet

are in good condition and free from damage,

d) Aircraft is not used for stall or single-engine training and

e) Repair is made within one flight day.


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3.


61 PROPELLERS 4. REMARKS OR EXCEPTIONS

1. Synchrophase System C 1 0 May be inoperative.

2. Reverse (REV) Captions C 2 1 One may be inoperative provided correct operation of Propeller is verified before takeoff.


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73 ENGINE FUEL & CONTROL 4. REMARKS OR EXCEPTIONS

1. Fuel Flow meters C 2 1 One may be inoperative provided: a) All other Engine Indicating Instruments

are operative and b) Both Fuel Quantity Gauges are

operative.

2. Fuel Pressure Warning Captions

C 2 1 May be inoperative provided associated Fuel Pressure Gauges and Fuel Flow meters are operative.

3. Fuel Manifold Purge System A 2 0 May be inoperative provided repairs are made within one flight day.


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74 IGNITION 4. REMARKS OR EXCEPTIONS

1. Continuous Ignition Systems

C 2 0 May be inoperative provided: a) Normal Ignition is unimpaired, b) Auto Re-Ignition System is installed

and verified to be operative, c) Jetstream SB 74JM7693A for the

Auto Re-Ignition System has been complied with and

d) Aircraft is not operated in known or forecast icing conditions.

2. Ignition Lights C 2 1 (O) One may be inoperative provided: a) Continuous Ignition is operative and

audibly checked prior to each flight and

b) Aircraft is not operated in known or forecast icing conditions.

3.

Auto Re-Ignition System C 2 0 Not installed on J31 For J32: May be inoperative provided: a) Normal Ignition is unimpaired and b) Continuous Ignition is operative and

selected: 1) During takeoff and climb out in actual

or potential icing conditions, 2) When ice is visible on or shedding from

propeller(s) spinner(s) or leading edge(s),

3) Immediately anytime Engine flameout occurs as a possible result of ice ingestion

4) During approach and landing while in or shortly following flight in actual or potential icing conditions and

5) When taking off on a slush covered runway.


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74 IGNITION 4. REMARKS OR EXCEPTIONS

3.

Auto Re-Ignition System (Cont)

NOTE: Potential icing conditions in precipitation or visible meteorological conditions: 1) Begin when the OAT is plus 5 degrees C

(plus 41 degrees F) or colder or 2) End when the OAT is plus 10 degrees C

(plus 50 degrees F) or warmer.


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76. ENGINE CONTROLS 4. REMARKS OR EXCEPTIONS

1. SRL System C 2 0 May be inoperative provided: a) AFM unconditioned EGT limits are not

exceeded, b) APR is in the OFF position, c) Inoperative SRL is OFF, d) Power Augmentation is not used and e) Water Methanol is not used except for

aircraft with BAE Mod. 7340 installed by BAE kit 3147/2 or kit 3358, for these aircraft; refer to AFM EGT limits with SRL Computer inoperative.

2. Torque and Temperature Limiters (TTL)

C 2 0 May be inoperative provided: a) AFM EGT and torque limitations are not

exceeded, b) APR/Water Methanol is OFF and c) Inoperative TTL is OFF.

3.

Automatic Performance Reserve (APR)

C 1 0 May be inoperative provided AFM performance data “Without APR” is used.

4.

Power Augmentation System

C 1 0 May be inoperative provided AFM performance data “Without Power Augmentation” is used.


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3.


79 ENGINE OIL 4. REMARKS OR EXCEPTIONS

1. Oil Cooler Flap OPEN/CLOSED Captions

C 2 0 (O) May be inoperative provided correct Oil Cooler Flap operation is verified prior to departure.

2. Oil Cooler Flap Auto Function

C 2 0 May be inoperative provided the manual functions are operative.

3. Oil Cooler Flap A 2 1 (M) (O) One may be inoperative in the CLOSED position provided:

a) Opposite side System operates normally, b) AFM performance is observed, c) Oil pressure and temperature limitations

as specified in the AFM are monitored, d) Affected System is deactivated and e) Operations are limited to not more than

three flight days before repair is made.

A 2 1 (M) (O) One may be inoperative in the OPEN position provided:

a) Opposite side System operates normally, b) Maximum air speed is 150 KIAS, c) Oil pressure limitations as specified in the

AFM are monitored, d) Minimum oil temperature for takeoff and

flight is +55 degrees C, e) Affected System is deactivated and f) Operations are limited to not more than

three flight days before repair is made.


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82 WATER INJECTION 4. REMARKS OR EXCEPTIONS

1.

Water Methanol System C 0 0 Not installed on Aircrafts

2.

Water Methanol Quantity Indicator System

C 0 0 Not installed on Aircrafts

3.

Water Methanol Pumps A 0 0 Not installed on Aircrafts


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