W DOC AIRBUS | AMM A320F

Removal of the Right Translating Sleeve Access Panels [PW11]


TASK 78-32-64-000-802-A
Removal of the Right Translating Sleeve Access Panels


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
ZONE: 400
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-00-00-860-833-A
Procedure to Prevent Engine Motoring
TASK 78-30-00-040-805-A
Deactivation of the Thrust Reverser System for Ground Maintenance
3. Job Set-up
Subtask 78-32-64-941-052-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Do the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833).
Subtask 78-32-64-040-051-A ** ON A/C NOT FOR ALL
B. Deactivation of the Thrust Reverser for Ground Maintenance
WARNING: YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE AN INJURY AND/OR DAMAGE.
   (1) Do the deactivation of the thrust reverser system for ground maintenance (Ref. AMM TASK 78-30-00-040-805).
   (2) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position.
4. Procedure
Subtask 78-32-64-020-051-A ** ON A/C NOT FOR ALL
A. Removal of the Right Translating Sleeve Access Panel (2), (3) or (4).
   (1) Remove the four bolts (1) that attach the access panel (2), (3) or (4) to the translating sleeve.
   (2) Remove the access panel (2), (3) or (4) from the translating sleeve.
[Rev.10 from 2021] 2026.04.01 03:33:40 UTC