Failure of the Control of the Fuel Shut-off Valve on Engine 2
TASK 76-12-00-810-811-A
Failure of the Control of the Fuel Shut-off Valve on Engine 2
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 76-12-00-710-068-A ** ON A/C NOT FOR ALL
Subtask 76-12-00-865-051-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:37:27 UTC
Failure of the Control of the Fuel Shut-off Valve on Engine 2
1. Possible Causes
- aircraft wiring
- RELAY-ENG/MASTER 2 [12QG]
- ACTUATOR-LP FUEL VALVE, ENG 2 [10QG]
- CTL SW-ENG/MASTER 2 [2KC]
- VALVE-LP FUEL, ENG 2 [13QM]
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 |
Subtask 76-12-00-710-068-A ** ON A/C NOT FOR ALL
A. Test
(1) Not applicable, the fault is evident.
4. Fault Isolation(1) Not applicable, the fault is evident.
Subtask 76-12-00-865-051-A ** ON A/C NOT FOR ALL
A. Table of the circuit breakers used in this procedure:
Subtask 76-12-00-810-059-B ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FUEL/LP VALVE/MOT1/ENG2 | 2QG | A09 |
| 49VU | ENGINE/2/HP FUEL SOV | 1KC2 | A02 |
| 121VU | FUEL/LP VALVE/MOT2/ENG2 | 4QG | M26 |
B. If the fault symptom is identified by the CFDS message MASTER LEVER, HMU:
Subtask 76-12-00-710-069-A ** ON A/C NOT FOR ALL - Make sure that the LP fuel valve is open AMM 28-24-00-710-002.
- 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 ASM 761201 and ASM 282401.
- Repair the above wiring or/and replace the RELAY-ENG/MASTER 2 [12QG] .
- Replace the ACTUATOR-LP FUEL VALVE, ENG 2 [10QG] AMM 28-24-51-000-001 and AMM 28-24-51-400-001.
- Do a check of the aircraft wiring between C/B (1KC2) pin 2 and CTL SW-ENG/MASTER 2 (2KC) pin 3G then CTL SW-ENG/MASTER 2 (2KC) pin 1G to HMU (HPSOV) connector A pin 1.
- Replace the CTL SW-ENG/MASTER 2 [2KC] on the panel 115VU AWM 761201 ESPM 204521.
- Replace the VALVE-LP FUEL, ENG 2 [13QM] AMM 28-24-41-000-001 and AMM 28-24-41-400-001.
C. Test
(1) Start the engine 2 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.
(1) Start the engine 2 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.