W DOC AIRBUS | AMM A320F

Installation of the Hinge Assembly


TASK 25-24-41-400-804-A
Installation of the Hinge Assembly


1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
Torque wrench: range to between 0.28 and 0.22 m.daN (24.78 and 19.47 lbf.in ) T
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 25-24-00-710-001-A
Adjustment of the Overhead Stowage Compartment Doors
TASK 25-24-41-400-002-A
Installation of the Door of the Overhead Stowage-Compartment
3. Job Set-up
Subtask 25-24-41-860-063-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
   (2) Make sure that the door is removed.
4. Procedure
Subtask 25-24-41-420-075-A ** ON A/C NOT FOR ALL
A. Installation of the Hinge Assembly
F Hinge Assembly ** ON A/C NOT FOR ALL
   (1) Put the hinge assembly (1) in position.
   (2) Install the washers (3) and the screws (2).
   (3) TORQUE the screws (2) to between 0.28 and 0.22 m.daN (24.78 and 19.47 lbf.in ) T.
   (4) Install the overhead stowage-compartment door (
Ref. AMM TASK 25-24-41-400-002).
Subtask 25-24-41-820-052-A ** ON A/C NOT FOR ALL
B. Adjustment of the Hinge assembly
   (1) If necessary, adjust the hinge assembly (1) (Ref. AMM TASK 25-24-00-710-001).
5. Close-up
Subtask 25-24-41-862-056-A ** ON A/C NOT FOR ALL
A. De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.03.31 23:32:16 UTC