Deactivation of the Flight Lock Actuator (FLA)
TASK 52-22-71-040-801-A
Deactivation of the Flight Lock Actuator (FLA)
MMEL 52-10-09C
FLIGHT LOCK ACTUATOR
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 52-22-71-860-069-A ** ON A/C NOT FOR ALL
Subtask 52-22-71-040-050-A ** ON A/C NOT FOR ALL 5. Close-up
Subtask 52-22-71-865-072-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:27:46 UTC
Deactivation of the Flight Lock Actuator (FLA)
Task Summary
1. Reason for the Job| Access | Test | Specific Tools | Mhr | E/T | Nb Men |
|---|---|---|---|---|---|
| YES | NO | NO | 1.0 | 1.0 | 1 |
MMEL 52-10-09C
FLIGHT LOCK ACTUATOR
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 833, 834, 843, 844 |
| 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 25-23-47-000-803-A | Removal of the Door Lining from the Overwing Emergency Exit |
| TASK 25-23-47-400-803-A | Installation of the Door Lining on the Overwing Emergency Exit |
| TASK 52-22-00-410-802-A | Closing of the Overwing Emergency-Exit Door from the Passenger Compartment |
| TASK 52-22-71-000-801-A | Removal of the Flight Lock Actuator (FLA) |
Subtask 52-22-71-860-069-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that applicable overwing emergency exit 833 ( 843) or 834 ( 844) is closed, latched and locked (Ref. AMM TASK 52-22-00-410-802).
Subtask 52-22-71-865-071-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that applicable overwing emergency exit 833 ( 843) or 834 ( 844) is closed, latched and locked (Ref. AMM TASK 52-22-00-410-802).
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 52-22-71-010-058-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | EIS/SDAC1 AND 2/DOOR/DET/PAX | 48WV | P05 |
| 122VU | FLIGHT LOCK OWD | 40WN | U16 |
C. Get Access
(1) Remove the lining of applicable overwing emergency exit 833 ( 843) or 834 ( 844) (Ref. AMM TASK 25-23-47-000-803).
4. Procedure(1) Remove the lining of applicable overwing emergency exit 833 ( 843) or 834 ( 844) (Ref. AMM TASK 25-23-47-000-803).
Subtask 52-22-71-040-050-A ** ON A/C NOT FOR ALL 5. Close-up
Subtask 52-22-71-865-072-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 52-22-71-410-058-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | EIS/SDAC1 AND 2/DOOR/DET/PAX | 48WV | P05 |
| 122VU | FLIGHT LOCK OWD | 40WN | U16 |
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the lining of applicable overwing emergency exit 833 ( 843) or 834 ( 844) (Ref. AMM TASK 25-23-47-400-803).
Subtask 52-22-71-860-070-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the lining of applicable overwing emergency exit 833 ( 843) or 834 ( 844) (Ref. AMM TASK 25-23-47-400-803).
C. Aircraft Maintenance Configuration
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.