Removal of the Access Door
TASK 57-51-37-000-008-A
Removal of the Access Door
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 57-51-37-941-064-A
Subtask 57-51-37-020-057-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:15:42 UTC
Removal of the Access Door
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
1. Reason for the Job- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| 98D27803500001 | 1 | LOCKING TOOL ZERO POS |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 27-00-00-480-002-A | Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000) |
| TASK 27-50-00-866-009-A | Retraction of the Flaps on the Ground |
| TASK 27-50-00-866-009-A-01 | Retraction of the Flaps/Slats on the Ground |
Subtask 57-51-37-941-064-A
A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 57-51-37-860-056-A (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
B. Aircraft Maintenance Configuration
(1) Make sure that the flaps are fully retracted (Ref. AMM TASK 27-50-00-866-009).
(2) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever (Ref. AMM TASK 27-00-00-480-002).
(3) Put a WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(4) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE below the applicable access door 574AB(674AB).
Subtask 57-51-37-865-050-A (1) Make sure that the flaps are fully retracted (Ref. AMM TASK 27-50-00-866-009).
(2) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever (Ref. AMM TASK 27-00-00-480-002).
(3) Put a WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(4) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE below the applicable access door 574AB(674AB).
C. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
Subtask 57-51-37-020-057-A ** ON A/C NOT FOR ALL
A. Removal of the Access Door 574AB(674AB)
(1) Hold the access door (1) and remove the screws (4). Carefully let the door open on the hinge.
(2) Hold the access door (1) and remove the nuts (3) and the bolts (2) from the hinge.
(3) Carefully remove the access door (1).
Subtask 57-51-37-020-057-B ** ON A/C NOT FOR ALL (1) Hold the access door (1) and remove the screws (4). Carefully let the door open on the hinge.
(2) Hold the access door (1) and remove the nuts (3) and the bolts (2) from the hinge.
(3) Carefully remove the access door (1).
A. Removal of the Access Door 574AB(674AB)
NOTE: The access door (1) is attached to the wing skin with two different lengths of screw. Make a record of the position of each screw as it is removed.
(1) Hold the access door (1) and remove the screws as follows: - the two screws (2)
- the eight screws (3).
Access Door 574AB(674AB) - Location and Detail