DOC AIRBUS | TSM A320FLoss of the Bleed Pressure Monitoring of the Engine 2
TASK 36-11-00-810-882-A
Loss of the Bleed Pressure Monitoring of the Engine 2
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 36-11-00-710-211-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 36-11-00-810-132-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:33:47 UTC
Loss of the Bleed Pressure Monitoring of the Engine 2
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 36-11-00-740-001 | BITE Test of the BMC 1(2) |
| AMM 36-11-16-000-001 | Removal of the Bleed Regulated Pressure-Transducer |
| AMM 36-11-16-400-001 | Installation of the Bleed Regulated Pressure-Transducer |
| AMM 36-11-34-000-001 | Removal of the BMC |
| AMM 36-11-34-400-001 | Installation of the BMC |
Subtask 36-11-00-710-211-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 36-11-00-810-132-A ** ON A/C NOT FOR ALL
A. If the test gives a maintenance message:
Subtask 36-11-00-710-212-A ** ON A/C NOT FOR ALL - Do the trouble shooting procedure related to the maintenance message.
- replace the XDCR-BLEED REGULATED PRESS, ENG 2 [8HA2] AMM 36-11-16-000-001 and AMM 36-11-16-400-001.
- replace the BMC-2 [1HA2] AMM 36-11-34-000-001 and AMM 36-11-34-400-001.
B. After the subsequent flight, make sure that the fault does not continue.