W DOC AIRBUS | TSM A320F

Fan Air Valve of the Engine 1 Failed


TASK 36-11-00-810-986-A
Fan Air Valve of the Engine 1 Failed


1. Possible Causes
  • VALVE-FAN AIR, ENG1 [9HA1]
  • wiring
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)
ASM 361101
AMM 36-11-54-000-802
Removal of the Fan Air-Valve Actuator
AMM 36-11-54-400-802
Installation of the Fan Air-Valve Actuator
AMM 36-11-54-720-804
Functional Test of the Opening of the Fan Air Valve with the Bleed Test Set P/N 98D36109001000
3. Fault Confirmation
Subtask 36-11-00-740-087-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the Bite test of the EBAS AMM 36-11-00-740-802.
4. Fault Isolation
Subtask 36-11-00-810-364-A ** ON A/C NOT FOR ALL
A. If the fault is identified by the maintenance message FAN AIR-V (9HA1):
   (1) Do a functional test of the Fan Air Valve (9HA1) AMM 36-11-54-720-804.
   (2) If the test confirms the fault:
     (a) Replace the VALVE-FAN AIR, ENG1 [9HA1] AMM 36-11-54-000-802 and AMM 36-11-54-400-802.
   (3) Do the test given in Para. 3.
Subtask 36-11-00-810-365-A ** ON A/C NOT FOR ALL
B. If the fault continues:
   (1) Do a check of the wiring from Fan Air Valve (9HA1) pin A/1 and A/2 to BMC1 (1HA1) pin AB/12C and AB/12B ASM 361101.
   (2) If the wiring is damaged:
     (a) Repair or replace the wiring .
Subtask 36-11-00-810-366-A ** ON A/C NOT FOR ALL
C. If the fault continues:
   (1) Do a check of the wiring from Fan Air Valve (9HA1) pin A/1 and A/2 to BMC2 (1HA2) pin AB/13C and AB/13B ASM 361101.
   (2) If the wiring is damaged:
     (a) Repair or replace the wiring .
Subtask 36-11-00-810-675-A ** ON A/C NOT FOR ALL
D. If the fault continues:
   (1) Do a check and repair the wiring between pin A/3 of the Fan Air Valve (9HA1) and the ground terminal.
[Rev.8 from Aug 2018] 2026.04.04 04:33:54 UTC