W DOC AIRBUS | TSM A320F

Skin Air-Inlet Valve Jammed or Air-Inlet Check Valve Failure


TASK 21-26-00-810-840-A
Skin Air-Inlet Valve Jammed or Air-Inlet Check Valve Failure


1. Possible Causes
  • CHECK VALVE-AIR INLET, AVNCS VENT [2150HM]
  • wiring
  • VALVE-SKIN AIR INLET, AVNCS VENT [15HQ]
  • AEVC [10HQ]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 21-26-00-710-001
Operational Check of the Avionics Equipment Ventilation-System via MCDU
AMM 21-26-00-710-008
Operational Test to Read the CFDS for CLASS 3 Faults of the AEVC
AMM 21-26-00-710-009
Operational Test to Read the CFDS for LAST LEG REPORT of the AEVC
ASM 212603
AMM 21-26-34-000-001
Removal of the Avionics Equipment Ventilation Computer (AEVC)
AMM 21-26-34-400-001
Installation of the Avionics Equipment Ventilation Computer (AEVC)
AMM 21-26-52-000-001
Removal of the Avionics-Ventilation Skin Air-Inlet-Valve
AMM 21-26-52-400-001
Installation of the Avionics-Ventilation Skin Air-Inlet-Valve
AMM 21-26-56-000-001
Removal of the Air Inlet Check Valve
AMM 21-26-56-280-002
Operational Check of Air Inlet Check Valve
AMM 21-26-56-400-001
Installation of the Air Inlet Check Valve
3. Fault Confirmation
Subtask 21-26-00-865-077-A
A. Table of the circuit breakers used in this procedure:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
122VUAIR COND/AVNCS/VENT/MONG3HQY17
Subtask 21-26-00-710-119-A
B. Test
   (1) Do the reset of the AEVC (10HQ).
     (a) Open the circuit breaker AIR COND/AVNCS/VENT/MONG (3HQ).
     (b) Wait for five seconds.
     (c) Close the circuit breaker AIR COND/AVNCS/VENT/MONG (3HQ).
   (2) Do the operational test of the avionics equipment ventilation from the Multipurpose Control and Display Unit (MCDU) AMM 21-26-00-710-001.
   (3) Read the LAST LEG REPORT of the AEVC AMM 21-26-00-710-009.
   (4) Read the CLASS 3 faults of the AEVC AMM 21-26-00-710-008.
4. Fault Isolation
Subtask 21-26-00-810-097-A
A. If the test is OK:
   (1) If the result of the operational check is not correct:
   (2) If the result of the operational check is correct:
  • Do a check of the wiring ASM 212603 between the AEVC (10HQ) and the skin air-inlet valve (15HQ):
    . Pin AA/4B and pin A/C
    . Pin AA/4A and pin A/A
    . Pin AB/4B and pin A/M
    . Pin AB/4A and pin A/J.
     (a) If the wiring is not correct:
  • Repair the wiring.
     (b) If the wiring is correct:
  • Do a check of the wiring ASM 212603 between the SDAC1 (1WV1) and SDAC2 (1WV2), and the skin air-inlet valve (15HQ):
    . Pin AD/11C and pin A/M
    . Pin AD/10F and pin A/J.
       1 If the wiring is not correct:
  • Repair the wiring.
       2 If the wiring is correct:
       3 If the fault continues:
Subtask 21-26-00-710-120-A
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:24:39 UTC