W DOC AIRBUS | TSM A320F

Fan Air Valve of the Engine 2 Failed


TASK 36-11-00-810-987-A
Fan Air Valve of the Engine 2 Failed


1. Possible Causes
  • VALVE-FAN AIR, ENG2 [9HA2]
  • 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 361102
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 36-11-00-740-088-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 36-11-00-810-367-A ** ON A/C NOT FOR ALL
A. If the fault is identified by the maintenance menssage FAN AIR-V (9HA2):
   (1) Do a functional test of the Fan Air Valve (9HA2) AMM 36-11-54-720-804.
   (2) If the test confirms the fault:
     (a) Replace the VALVE-FAN AIR, ENG2 [9HA2] AMM 36-11-54-000-802 and AMM 36-11-54-400-802.
   (3) Do the test given in Para. 3.
Subtask 36-11-00-810-368-A ** ON A/C NOT FOR ALL
B. If the fault continues:
   (1) Do a check of the wiring from Fan Air Valve (9HA2) pin A/1 and A/2 to BMC2 (1HA2) pin AB/12C and AB/12B ASM 361102.
   (2) If the wiring is damaged:
     (a) Repair or replace the wiring .
Subtask 36-11-00-810-369-A ** ON A/C NOT FOR ALL
C. If the fault continues:
   (1) Do a check of the wiring from Fan Air Valve (9HA2) pin A/1 and A/2 to BMC1 (1HA1) pin AB/13C and AB/13B ASM 361102.
   (2) If the wiring is damaged:
     (a) Repair or replace the wiring .
Subtask 36-11-00-810-676-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