DOC AIRBUS | TSM A320FFailure of the Overpressure Valve in Closed Position on the Engine 2
TASK 36-11-00-810-946-A
Failure of the Overpressure Valve in Closed Position on the Engine 2
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 36-11-00-720-053-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 36-11-00-810-240-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:33:50 UTC
Failure of the Overpressure Valve in Closed Position on the Engine 2
1. Possible Causes
- VALVE-OVERPRESSURE, ENG 2 [5HA2]
- wiring
- VALVE-HP BLEED [4000HA]
- sense line
sense line between the bleed pressure-regulator valve (4001HA) and the HP bleed valve (4000HA) - VALVE-BLEED PRESS REG [4001HA]
sense line between the bleed pressure regulator valve (4001HA) and the HP bleed valve (4000HA)
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| ASM 361102 | |
| AMM 36-11-49-000-029 | Removal of the Pneumatic Sense Lines in the Pylon |
| AMM 36-11-49-000-042 | Removal of the Pylon Interface Duct |
| AMM 36-11-49-400-029 | Installation of the Pneumatic Sense Lines in the Pylon |
| AMM 36-11-49-400-042 | Installation of the Pylon Interface Duct |
| AMM 36-11-51-000-040 | Removal of the High Pressure Bleed Valve |
| AMM 36-11-51-000-042 | Removal of the High Pressure Bleed Valve |
| AMM 36-11-51-400-040 | Installation of the High Pressure Bleed Valve |
| AMM 36-11-51-400-042 | Installation of the High Pressure Bleed Valve |
| AMM 36-11-52-000-040 | Removal of the Bleed Pressure-Regulator Valve |
| AMM 36-11-52-000-042 | Removal of the Bleed Pressure Regulator Valve |
| AMM 36-11-52-400-040 | Installation of the Bleed Pressure-Regulator Valve |
| AMM 36-11-52-400-042 | Installation of the Bleed Pressure Regulator Valve |
| AMM 36-11-53-000-001 | Removal of the Overpressure Valve |
| AMM 36-11-53-400-001 | Installation of the Overpressure Valve |
| AMM 36-11-53-720-001 | Functional Test of the Overpressure Valves with the Bleed Test Set P/N 98D36003000000 |
Subtask 36-11-00-720-053-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 36-11-00-810-240-A ** ON A/C NOT FOR ALL
A. If the functional test of the engine 2 overpressure valve (5HA2) is not correct:
Subtask 36-11-00-810-242-A ** ON A/C NOT FOR ALL - replace the VALVE-OVERPRESSURE, ENG 2 [5HA2] AMM 36-11-53-000-001 and AMM 36-11-53-400-001.
- do a check and repair the wiring between:
. pin A/1 of the engine 2 overpressure valve (5HA2) and pin AA/10A of the BMC2 (1HA2)
. pin A/2 of the engine 2 overpressure valve and the ground ASM 361102.
B. If the functional test of the engine 2 overpressure valve (5HA2) is correct:
Subtask 36-11-00-810-242-C ** ON A/C NOT FOR ALL - replace the VALVE-HP BLEED [4000HA] AMM 36-11-51-000-040 and AMM 36-11-51-400-040.
- do a leak check on the sense line between the bleed pressure regulator valve (4001HA) and the HP bleed valve (4000HA).
- repair or replace the
sense line between the bleed pressure-regulator valve (4001HA) and the HP bleed valve (4000HA) AMM 36-11-49-000-029 and AMM 36-11-49-400-029.
- replace the VALVE-BLEED PRESS REG [4001HA] AMM 36-11-52-000-040 and AMM 36-11-52-400-040.
B. If the functional test of the engine 2 overpressure valve (5HA2) is correct:
Subtask 36-11-00-720-054-A ** ON A/C NOT FOR ALL - replace the VALVE-HP BLEED [4000HA] AMM 36-11-51-000-042 and AMM 36-11-51-400-042.
- do a leak check on the sense line between the bleed pressure regulator valve (4001HA) and the HP bleed valve (4000HA).
- repair or replace the
sense line between the bleed pressure regulator valve (4001HA) and the HP bleed valve (4000HA) AMM 36-11-49-000-042 and AMM 36-11-49-400-042.
- replace the VALVE-BLEED PRESS REG [4001HA] AMM 36-11-52-000-042 and AMM 36-11-52-400-042.
C. After the subsequent flight, make sure that the fault does not continue.