Removal of the Locking Hook
TASK 52-22-61-000-801-A
Removal of the Locking Hook
1. Reason for the Job
Self explanatory
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 52-22-61-860-050-A ** ON A/C NOT FOR ALL
Subtask 52-22-61-020-051-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:27:44 UTC
Removal of the Locking Hook
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | SCRAPER - NON METALLIC |
| 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 25-23-44-000-001-A | Removal of the Lower Sidewall Panels (Dado Panels) |
| TASK 25-23-47-000-803-A | Removal of the Door Lining from the Overwing Emergency Exit |
| TASK 25-62-00-481-001-A | Special Precautions before Work on the Offwing Escape-Slide Systems |
| TASK 52-22-00-010-802-A | Opening of the Overwing Emergency-Exit Door from the Passenger Compartment |
Subtask 52-22-61-860-050-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).
Subtask 52-22-61-865-050-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 52-22-61-010-050-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | EIS/SLIDES/ARM AND WARN/FLT | 15WN | P11 |
| 121VU | EIS/SLIDES/ARM AND WARN/GND | 13WN | P10 |
| 121VU | EIS/SDAC1 AND 2/DOOR/DET/PAX | 48WV | P05 |
| 122VU | FLIGHT LOCK OWD | 40WN | U16 |
C. Get Access
(1) Obey the special precautions before you work on the offwing escape-slide systems (Ref. AMM TASK 25-62-00-481-001).
(2) Open applicable overwing emergency-exit door 833 ( 843) or 834 ( 844) (Ref. AMM TASK 52-22-00-010-802).
(3) Remove related cover 241ADW (242ADW) or 241AEW (242AEW) (Ref. AMM TASK 25-23-47-000-803).
(4) Remove the adjacent lower sidewall panel (dado panels) (Ref. AMM TASK 25-23-44-000-001).
4. Procedure(1) Obey the special precautions before you work on the offwing escape-slide systems (Ref. AMM TASK 25-62-00-481-001).
(2) Open applicable overwing emergency-exit door 833 ( 843) or 834 ( 844) (Ref. AMM TASK 52-22-00-010-802).
(3) Remove related cover 241ADW (242ADW) or 241AEW (242AEW) (Ref. AMM TASK 25-23-47-000-803).
(4) Remove the adjacent lower sidewall panel (dado panels) (Ref. AMM TASK 25-23-44-000-001).
Subtask 52-22-61-020-051-A ** ON A/C NOT FOR ALL
A. Removal of the Locking Hook
(1) Use the SCRAPER - NON METALLIC to remove the sealant (7):
(3) Remove the locking hook (3) and the plate (4) from the structure (8).
(1) Use the SCRAPER - NON METALLIC to remove the sealant (7):
- Around the locking hook (3) and the plate (4)
- On the heads of the bolts (1) and the nuts (5).
(3) Remove the locking hook (3) and the plate (4) from the structure (8).
Locking Hooks