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
A. Referenced Information
3. Fault Confirmation
Subtask 21-26-00-865-077-A
Subtask 21-26-00-810-097-A
[Rev.8 from Aug 2018]
2026.04.04 04:24:39 UTC
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]
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 |
Subtask 21-26-00-865-077-A
A. Table of the circuit breakers used in this procedure:
Subtask 21-26-00-710-119-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 122VU | AIR COND/AVNCS/VENT/MONG | 3HQ | Y17 |
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(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.
Subtask 21-26-00-810-097-A
A. If the test is OK:
Subtask 21-26-00-710-120-A - Do the operational check of the air inlet check-valve (2150HM) AMM 21-26-56-280-002.
- Replace the CHECK VALVE-AIR INLET, AVNCS VENT [2150HM] AMM 21-26-56-000-001 and AMM 21-26-56-400-001.
- 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.
- Repair the wiring.
- 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.
- Repair the wiring.
- Replace the VALVE-SKIN AIR INLET, AVNCS VENT [15HQ] AMM 21-26-52-000-001 and AMM 21-26-52-400-001.
- Replace the AEVC [10HQ] AMM 21-26-34-000-001 and AMM 21-26-34-400-001.
B. Do the test given in Para. 3.