Failure of the Skin Exchanger Isolation-Valve
TASK 21-26-00-810-807-A
Failure of the Skin Exchanger Isolation-Valve
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 21-26-00-865-062-A
Subtask 21-26-00-810-071-A
[Rev.8 from Aug 2018]
2026.04.04 04:38:49 UTC
Failure of the Skin Exchanger Isolation-Valve
1. Possible Causes
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 212602 | |
| 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 21-26-55-000-002 | Removal of the Avionics Ventilation Skin Exchanger Isolation Valve |
| AMM 21-26-55-400-002 | Installation of the Avionics Ventilation Skin Exchanger Isolation Valve |
Subtask 21-26-00-865-062-A
A. Table of the circuit breakers used in this procedure:
Subtask 21-26-00-710-088-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 21-26-00-810-071-A
A. If the test gives the maintenance message ISOL V 24HQ:
Subtask 21-26-00-710-089-A - Do a check of the status of the skin exchanger isolation-valve (24HQ) microswitches, between pin A/J and pin A/G and between pin A/M and pin A/K ASM 212602.
- Replace the VALVE-SKIN EXCHANGER ISOL, AVNCS VENT [24HQ] AMM 21-26-55-000-002 and AMM 21-26-55-400-002.
- Do a check for a ground signal at pin A/U, pin A/G and pin A/K of the skin exchanger isolation-valve (24HQ) ASM 212602.
- Repair the related wiring .
- Do a check of the wiring between the AEVC (10HQ) and the skin exchanger isolation-valve (24HQ) ASM 212602:
. Pin AB/5A and pin A/J
. Pin AB/5B and pin A/M.
- Repair the related wiring .
- Do a check of the wiring between the AEVC (10HQ) and the skin exchanger isolation-valve (24HQ) ASM 212602:
. Pin AA/5A and pin A/A
. Pin AA/5B and pin A/C.
- Repair the related wiring .
- Replace the VALVE-SKIN EXCHANGER ISOL, AVNCS VENT [24HQ] AMM 21-26-55-000-002 and AMM 21-26-55-400-002.
- Replace the AEVC [10HQ] AMM 21-26-34-000-001 and AMM 21-26-34-400-001.
B. Do the operational test given in Para. 3.