Reactivation of the Avionics Equipment Ventilation Computer (AEVC)
TASK 21-26-00-440-005-A
Reactivation of the Avionics Equipment Ventilation Computer (AEVC)
1. Reason for the Job
MMEL 21-26-10A
AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC)
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 21-26-00-861-078-A
Subtask 21-26-00-440-050-A
Subtask 21-26-00-941-091-A
[Rev.10 from 2021]
2026.04.02 06:10:59 UTC
Reactivation of the Avionics Equipment Ventilation Computer (AEVC)
1. Reason for the Job
MMEL 21-26-10A
AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC)
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 824 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 52-41-00-010-002-A | Open the Avionics Compartment Doors for Access |
| TASK 52-41-00-410-002-A | Close the Avionics Compartment Doors after Access |
Subtask 21-26-00-861-078-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 21-26-00-010-099-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
B. Get Access
(1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 824.
(2) Open the access door 824 (Ref. AMM TASK 52-41-00-010-002).
4. Procedure(1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 824.
(2) Open the access door 824 (Ref. AMM TASK 52-41-00-010-002).
Subtask 21-26-00-440-050-A
A. Reactivation of the skin air inlet valve
(1) On the VENTILATION section of the overhead panel 22VU:
5. Close-up(1) On the VENTILATION section of the overhead panel 22VU:
- push the BLOWER and EXTRACT pushbutton switches (on the EXTRACT pushbutton switch, the OVRD legend goes off on the BLOWER pushbutton switch, the FAULT LEGEND is on).
- push the PUSH latch to release the handle
- pull the handle and set the deactivation switch to ON
- put the handle back to its initial position and latch it.
Subtask 21-26-00-941-091-A
A. Aircraft Maintenance Configuration
(1) Remove the WARNING NOTICE(S).
Subtask 21-26-00-410-096-A (1) Remove the WARNING NOTICE(S).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access door 824 (Ref. AMM TASK 52-41-00-410-002).
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
Subtask 21-26-00-862-078-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access door 824 (Ref. AMM TASK 52-41-00-410-002).
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
Skin Air-Inlet Valve