W DOC AIRBUS | TSM A320F

High Bleed Temperature of Engine 1 in Climb


TASK 36-11-00-810-A37-A
High Bleed Temperature of Engine 1 in Climb


1. Possible Causes
  • EXCHANGER-BLEED AIR PRECOOL [7150HM1]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 36-11-00-740-802
BITE Test of the Engine Bleed Air System (EBAS) (System Test)
AMM 36-11-42-000-802
Removal of the Bleed-Air Precooler Exchanger
AMM 36-11-42-400-802
Installation of the Bleed-Air Precooler Exchanger
3. Fault Confirmation
Subtask 36-11-00-710-501-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test EBAS AMM 36-11-00-740-802.
4. Fault Isolation
Subtask 36-11-00-810-521-A ** ON A/C NOT FOR ALL
A. If the test gives a maintenance message:
  • Do the trouble shooting procedure related to the maintenance message.
   (1) If there is no maintenance message
     (a) Replace EXCHANGER-BLEED AIR PRECOOL [7150HM1] AMM 36-11-42-000-802 AMM 36-11-42-400-802.
Subtask 36-11-00-710-502-A ** ON A/C NOT FOR ALL
B. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:33:58 UTC