DOC AIRBUS | TSM A320FHigh Bleed Temperature of the Engine 1 in Descent
TASK 36-11-00-810-A25-A
High Bleed Temperature of the Engine 1 in Descent
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 36-11-00-710-480-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 36-11-00-810-480-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:33:57 UTC
High Bleed Temperature of the Engine 1 in Descent
1. Possible Causes
- SENSOR-EXCHANGER OUT TEMP, ENG 1 [6HA1]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 36-11-00-740-802 | BITE Test of the Engine Bleed Air System (EBAS) (System Test) |
| AMM 36-11-17-000-001 | Removal of the Heat-Exchanger Outlet-Temperature Sensor |
| AMM 36-11-17-400-001 | Installation of the Heat-Exchanger Outlet-Temperature Sensor |
Subtask 36-11-00-710-480-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 36-11-00-810-480-A ** ON A/C NOT FOR ALL
A. If the test gives a maintenance message:
Subtask 36-11-00-710-481-A ** ON A/C NOT FOR ALL - Do the trouble shooting procedure related to the maintenance message.
- Replace SENSOR-EXCHANGER OUT TEMP, ENG 1 [6HA1] AMM 36-11-17-000-001 and AMM 36-11-17-400-001.
B. After the subsequent flight, make sure that the fault does not continue.