W DOC AIRBUS | AMM A320F

Removal of the Reduction Gearbox


TASK 32-33-15-000-001-A
Removal of the Reduction Gearbox


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
Self explanatory
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
SHIM - WOODEN
No specific
AR
WARNING NOTICE(S)
98A27801001000
1
RIGGING PIN
98A27901002000
1
PIN-RIGGING,RUDDER CONTROL
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
211FF, 822
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 32-00-00-481-001-A
Installation of the Safety Devices on the Landing Gears
TASK 32-22-00-010-001-A
Nose Gear Doors - Ground Doors Opening
TASK 53-12-11-000-001-A
Removal of the Cockpit Floor Panels from FR1 thru FR12
3. Job Set-up
Subtask 32-33-15-941-050-A
A. Safety Precautions
   (1) In the cockpit, on the panel 400VU put WARNING NOTICE(S) in position to tell persons not to operate the landing gear control lever.
   (2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
   (3) On the panel 110VU, make sure that the free fall control handle is folded into the center console.
   (4) Install SHIM - WOODEN on each side of the free fall control handle to lock the handle in position.
Subtask 32-33-15-010-050-A
B. Get Access
   (1) Open the NLG doors (Ref. AMM TASK 32-22-00-010-001).
   (2) Open the lateral avionics-compartment door 822.
   (3) Remove the cockpit floor panel 211FF (Ref. AMM TASK 53-12-11-000-001).
   (4) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position in zone 123.
   (5) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position below the lateral avionics-compartment door 822.
Subtask 32-33-15-480-050-A
C. Installation of the Rigging Pins
   (1) In the nose landing gear well, put the tool 98A27901002000 PIN-RIGGING,RUDDER CONTROL (9) in the bottom bellcrank (10).
   (2) Put the 98A27801001000 RIGGING PIN (1) in position to lock the quadrant (2).
4. Procedure
Subtask 32-33-15-020-050-A
A. Removal of the Free Fall Reduction Gearbox
   (1) Remove the cotter pin (15), the nut (14) and the washer (13).
   (2) Remove the screw (5) and disconnect the rod (8).
   (3) Cut and remove the lockwire from the screw (19). Remove the screw (19) and the washer (18).
   (4) Remove the cotter pin (20), the nut (21) and the washer (22).
   (5) Remove the cable guide (23) and the shims (24) and (17).
   (6) Remove the pins (12) from the cable tension adjusters (11).
   (7) To do this, turn the cable tension adjusters (11).
Decrease the tension to release the cable reels (29) and (31).
   (8) Remove the cables (29) and (31) from the gearbox (3). Attach the cables to the structure.
   (9) Remove the nuts (16) and the bolts (4).
   (10) Remove the free fall gearbox (3) from its support and remove the screw (30).
[Rev.10 from 2021] 2026.04.01 00:46:36 UTC