W DOC AIRBUS | AMM A320F

Removal of the NLG Aft Door-Assembly for Access


TASK 32-22-13-010-001-A
Removal of the NLG Aft Door-Assembly for Access


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: MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
1. Reason for the Job
This procedure is only applicable when the NLG aft door-assembly is removed for access. For the procedure applicable to the removal of the NLG aft door-assembly for replacement, refer to TASK 32-22-13-000-001.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
SAFETY BARRIER(S)
No specific
AR
WARNING NOTICE(S)
 B. Referenced Information
REFERENCE
DESIGNATION
F NLG Aft Door-Assembly ** ON A/C NOT FOR ALL
F NLG Aft Door-Assembly ** ON A/C NOT FOR ALL
F NLG Aft Door-Assembly ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 32-22-13-860-053-A
A. Aircraft Maintenance Configuration
   (1) In the cockpit, on panel 400VU, put the WARNING NOTICE(S) in position to tell persons not to operate the landing gear control-lever.
   (2) Put the SAFETY BARRIER(S) in position.
   (3) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position.
4. Procedure
Subtask 32-22-13-020-054-A ** ON A/C NOT FOR ALL
A. Removal of the NLG Aft Door-Assembly
NOTE: Do not change the adjustment of the rotating rod (1).
   (1) Remove the nuts (18) and (2) and the bolts (11) and (3).
   (2) Remove the bonding braids (12) and (4).
   (3) Remove the cotter pin (19) and discard it.
   (4) Remove the nut (20) and the washer (21).
   (5) Remove the bolt (23) and release the door (22) from its connection to the rotating rod (1).
   (6) Remove the cotter pin (16) and discard it.
   (7) Remove the nut (17), washer (15) and bolt (13).
NOTE: Keep the door (22) in position to help you remove the second hinge assembly.
   (8) Remove the cotter pin (5) and discard it.
   (9) Remove the nut (6), washer (7) and bolt (10).
   (10) Remove the door (22).
   (11) Remove the bushes (8) and (9) from the aft hinge of the door (22).
   (12) Remove the bush (14) from the aircraft structure fitting.
Subtask 32-22-13-020-054-B ** ON A/C NOT FOR ALL
A. Removal of the Aft Door Assy
NOTE: Do not change the adjustment of the rotating rod (1).
   (1) Remove the nuts (22) and (3) and the bolts (14) and (4).
   (2) Remove the bonding braids (15) and (5).
   (3) Remove the nuts (2), the jumpers (11) and (17) and the bolts (13).
   (4) Remove the cotter pin (23) and discard it, remove the nut (24) and the washer (25).
   (5) Remove the bolt (27) and release the door (26) from its connection to the rotating rod (1).
   (6) Remove the cotter pin (20) and discard it, remove the nut (21), the bolt (16), the washer (18) and the two shouldered bushes (19).
NOTE: Keep the door (26) in position to help you to remove the second hinge assembly.
   (7) Remove the cotter pin (6) and discard it, remove the nut (7), the bolt (12), the washer (10) and the bushes (8) and (9).
   (8) Remove the door (26).
[Rev.10 from 2021] 2026.04.01 00:43:18 UTC