W DOC AIRBUS | TSM A320F

Failure of the Control of the Fuel Shut-off Valve on Engine 1


TASK 76-12-00-810-810-A
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]
  • CTL SW-ENG/MASTER 1 [3KC]
  • VALVE-LP FUEL, ENG 1 [12QM]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ESPM 204521
AMM 28-24-00-710-002
Operational Test of the ENG 1(2) LP Fuel Valve
ASM 282401
AMM 28-24-41-000-001
Removal of the LP Fuel Valve
AMM 28-24-41-400-001
Installation of the LP Fuel Valve
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 761201
AWM 761201
3. Fault Confirmation
Subtask 76-12-00-710-066-A ** ON A/C NOT FOR ALL
A. Test
   (1) Not applicable, the fault is evident.
4. Fault Isolation
Subtask 76-12-00-865-050-A ** ON A/C NOT FOR ALL
A. Table of the circuit breakers used in this procedure:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFUEL/LP VALVE/MOT1/ENG11QGA08
49VUENGINE/1/HP FUEL SOV1KC1A01
121VUFUEL/LP VALVE/MOT2/ENG13QGM25
Subtask 76-12-00-810-058-B ** ON A/C NOT FOR ALL
B. If the fault symptom is identified by the CFDS message MASTER LEVER, HMU:
   (1) If the valve is not open:
  • Do a check of the aircraft wiring between the circuit breakers (1QG), (3QG) and the ENG 1 LP fuel valve actuator (9QG) pins AA/A, BB/A ASM 761201 and ASM 282401.
     (a) If there is no continuity:
  • Repair the above wiring or/and replace the RELAY-ENG/MASTER 1 [11QG] .
     (b) If there is continuity:
     (c) If the valve is open:
  • Do a check of the aircraft wiring between C/B (1KC1) pin 2 and CTL SW-ENG/MASTER 1 (3KC) pin 3G then CTL SW-ENG/MASTER 1 (3KC) pin 1G to HMU (HPSOV) connector A pin 1.
     (d) If the fault continues:
     (e) If the fault continues:
Subtask 76-12-00-710-067-A ** ON A/C NOT FOR ALL
C. Test
   (1) Start the engine 1 by the engine automatic start procedure AMM 71-00-00-710-003.
   (2) Make sure that there is no ECAM and CFDS fault message shown.
[Rev.8 from Aug 2018] 2026.04.04 04:37:27 UTC