Removal of the Cabin Window of the Overwing Emergency-Exit Door
TASK 56-31-65-000-801-A
Removal of the Cabin Window of the Overwing Emergency-Exit Door
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 56-31-65-860-051-A ** ON A/C NOT FOR ALL
Subtask 56-31-65-020-050-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:08:07 UTC
Removal of the Cabin Window of the Overwing Emergency-Exit Door
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT) |
| No specific | 1 | GLOVES - COTTON, LINT-FREE, CLEAN |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| 98D27803000000 | 1 | LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 833, 834, 843, 844 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-00-00-481-002-A | Installation of the Wingrip |
| 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 25-23-47-000-803-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 27-00-00-480-002-A | Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000) |
| TASK 52-22-00-710-802-A | Operational Check of Escape Slide Release Mechanism |
Subtask 56-31-65-860-051-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) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever (Ref. AMM TASK 27-00-00-480-002).
(3) Obey the special precautions before you start the work on the offwing escape-slide systems (Ref. AMM TASK 25-62-00-481-001).
Subtask 56-31-65-865-053-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever (Ref. AMM TASK 27-00-00-480-002).
(3) Obey the special precautions before you start the work on the offwing escape-slide systems (Ref. AMM TASK 25-62-00-481-001).
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 56-31-65-010-050-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| 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 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| 122VU | FLIGHT LOCK OWD | 40WN | U16 |
C. Get Access
(1) Put on a safety harness:
(b) Put on and attach a safety harness before you start the work in the work area.
(2) Put the ACCESS PLATFORM 3M (10 FT) in position below applicable overwing emergency-exit door 833 ( 843) or 834 ( 844).
(3) Make sure that applicable overwing emergency-exit door 833 ( 843) or 834 ( 844) closed, latched and locked.
(4) Make sure that the overwing emergency-exit door is disarmed (Ref. AMM TASK 52-22-00-710-802).
(5) Remove the adjacent door linings (Ref. AMM TASK 25-23-47-000-803).
4. Procedure(1) Put on a safety harness:
WARNING:
YOU MUST PUT ON AND ATTACH A SAFETY HARNESS BEFORE YOU START WORK:
(a) If you do the work on the wings, install the individual pad system (Ref. AMM TASK 12-00-00-481-002). - ON THE THS OR IN THE REAR FUSELAGE
- ON TOP OF THE WINGS OR PYLONS.
(b) Put on and attach a safety harness before you start the work in the work area.
(2) Put the ACCESS PLATFORM 3M (10 FT) in position below applicable overwing emergency-exit door 833 ( 843) or 834 ( 844).
(3) Make sure that applicable overwing emergency-exit door 833 ( 843) or 834 ( 844) closed, latched and locked.
(4) Make sure that the overwing emergency-exit door is disarmed (Ref. AMM TASK 52-22-00-710-802).
(5) Remove the adjacent door linings (Ref. AMM TASK 25-23-47-000-803).
Subtask 56-31-65-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the Cabin Window
(2) Remove the retainer (3) from the cabin window (2).
(3) Carefully remove the cabin window (2) from the window frame (1).
NOTE: It is important to put on GLOVES - COTTON, LINT-FREE, CLEAN when you touch the window panes, components and assemblies.
(1) Loosen the nuts (4) and remove them. (2) Remove the retainer (3) from the cabin window (2).
(3) Carefully remove the cabin window (2) from the window frame (1).
Cabin Window - Overwing Emergency-Exit Door