- RELAY-ENG/MASTER 2 (12QG)

 - ACTUATOR-LP FUEL VALVE, ENG 2 (10QG)

 - VALVE-LP FUEL, ENG 2 (13QM)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM 28-24-00-710-002 Operational Test of the ENG 1(2) LP Fuel Valve 12QM
 (13QM)
R  AMM 28-24-41-000-001 Removal of the LP Fuel Valve 12QM(13QM)
R  AMM 28-24-41-400-001 Installation of the LP Fuel Valve 12QM(13QM) AMM 28-24-51-000-001 Removal of the LP Fuel Valve Actuator AMM 28-24-51-400-001 Installation of the LP Fuel Valve Actuator AMM 71-00-00-710-003 Engine Automatic Start ASM 28-24/01 ASM 76-12/01
 3. Fault Confirmation
__________________
 A. Test
 (1) Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/LP VALVE/MOT1/ENG2 2QG A09 121VU FUEL/LP VALVE/MOT2/ENG2 4QG M26
 F 『 EEFF : ALL E ∞∞76-12-00∞∞∞∞∞∞∞∞∞∞Page 207
 E E Nov 01/00 E E ECES
E B. If the fault symptom is identified by the CFDS message MASTER LEVER, HMU:

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 E  C F M  E
 E  E
 E  56  E
 E  E

 - make sure that the LP fuel valve is open (Ref. AMM TASK 28-24-00-710-002).
 (1) If the valve is not open:
 - do a check of the aircraft wiring between the circuit breakers (2QG), (4QG) and the ENG 2 LP fuel valve actuator (10QG) pins AA/A, BB/A (Ref. ASM 76-12/01) and (Ref. ASM 28-24/01).
 (a) If there is no continuity:

 - repair the above wiring or/and replace the RELAY-ENG/MASTER 2 (12QG).

 (b) If there is continuity:

 - replace the ACTUATOR-LP FUEL VALVE, ENG 2 (10QG) (Ref. AMM TASK 28-24-51-000-001) and (Ref. AMM TASK 28-24-51-400-001).

 (c) If the fault continues:

 - replace the VALVE-LP FUEL, ENG 2 (13QM) (Ref. AMM TASK 28-24-41-000-001) and (Ref. AMM TASK 28-24-41-400-001).
 C. Test
 (1) Start the engine 2 by the engine automatic start procedure (Ref. AMM TASK 71-00-00-710-003).

 (2) Make sure that there is no ECAM and CFDS fault message shown.

 F 『 EEFF : ALL E ∞∞76-12-00∞∞∞∞∞∞∞∞∞∞Page 208
 E E Feb 01/98 E E ECES
E

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 TASK 76-12-00-810-812
 Failure of the Control of the Fuel Shut-off Valve on Engine 1
 1. Possible Causes
_______________
 - aircraft wiring

 - RELAY-ENG/MASTER 1 (11QG)

 - ACTUATOR-LP FUEL VALVE, ENG 1 (9QG)

 - VALVE-LP FUEL, ENG 1 (12QM)

 - CTL SW-ENG/MASTER 1 (3KC)

 - fuel pump and filter assembly

 - HMU

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-24-00-710-002 Operational Test of the ENG 1(2) LP Fuel Valve 12QM
 (13QM) R AMM 28-24-41-000-001 Removal of the LP Fuel Valve 12QM(13QM) R AMM 28-24-41-400-001 Installation of the LP Fuel Valve 12QM(13QM)
 AMM 28-24-51-000-001 Removal of the LP Fuel Valve Actuator AMM 28-24-51-400-001 Installation of the LP Fuel Valve Actuator AMM 71-00-00-710-003 Engine Automatic Start AMM 73-11-10-000-003 Removal of the Fuel Pump and Filter Assembly AMM 73-11-10-400-003 Installation of the Fuel Pump and Filter Assembly AMM 73-21-10-000-002 Removal of the Hydromechanical Unit (HMU) AMM 73-21-10-400-002 Installation of the Hydromechanical Unit (HMU) ASM 28-24/01 ASM 76-12/01
 3. Fault Confirmation
__________________
 A. Test
 (1) Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/LP VALVE/MOT1/ENG1 1QG A08 121VU FUEL/LP VALVE/MOT2/ENG1 3QG M25
　
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