W DOC AIRBUS | AMM A320F

Removal of the Bearing from the Thrust-Reverser Cowl Hinge-Fitting at RIB3


TASK 54-57-17-000-808-A
Removal of the Bearing from the Thrust-Reverser Cowl Hinge-Fitting at RIB3


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.
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.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
CAUTION: BEFORE YOU INSTALL/REMOVE THE GSE-TOOL, READ THE INSTRUCTIONS IN THE APPLICABLE GSE INSTRUCTION MANUAL. WHILE YOU OPERATE THIS TOOL, CAREFULLY OBEY THEM. IF YOU DO NOT OBEY THE INSTRUCTIONS, DAMAGE TO EQUIPMENT CAN OCCUR.
ZONE: 415
ZONE: 425
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 3M (10 FT)- ADJUSTABLE
No specific
AR
WARNING NOTICE(S)
98D54003022000
1
RI BALL BEARING
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
415
LOWER PYLON
425
LOWER PYLON
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
451AL, 452AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
461AL, 462AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 78-30-00-040-807-A
Deactivation of the Thrust Reverser System for Nacelle Maintenance (ICU)
TASK 78-32-11-000-803-A
Removal of the Thrust Reverser Cowl Doors
3. Job Set-up
Subtask 54-57-17-941-066-A
A. Safety Precautions
   (1) On the center pedestal, on ENG panel 115VU:
     (a) Make sure that the ENG/MODE selector switch is in the NORM position.
     (b) Make sure that the ENG/MASTER 1(2) control switch is in the OFF position not less than five minutes before you do this procedure.
     (c) Put the WARNING NOTICE(S) in position to tell persons not to operate the ENG/MODE selector switch and the ENG/MASTER 1(2) control switch.
   (2) On the ENG section of maintenance panel 50VU:
     (a) Make sure that the ON legend of the FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put the WARNING NOTICE(S) in position to tell persons not to energize FADEC 1(2).
Subtask 54-57-17-040-060-A
B. Deactivation of the Thrust Reverser
WARNING: MAKE SURE THAT THE THRUST REVERSER IS LOCKED. IF NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY TO PERSONNEL AND/OR DAMAGE TO THE REVERSER.
   (1) Make the applicable thrust reverser unserviceable for maintenance (Ref. AMM TASK 78-30-00-040-807).
Subtask 54-57-17-010-065-A
C. Get Access
   (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position:
     (a) For the left pylon, at zone 415
     (b) For the right pylon, at zone 425.
   (2) Remove the applicable thrust-reverser cowl door (Ref. AMM TASK 78-32-11-000-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
4. Procedure
Subtask 54-57-17-020-065-A
A. Removal of the Bearing from the Thrust-Reverser Cowl Hinge-Fitting at RIB3
NOTE: The bearing (9) of the thrust-reverser cowl hinge-fitting (2) has one outer ring (1), one tabwasher (3) and one slotted nut (4).
The outer ring (1) has an inner bush.
   (1) To remove the bearing (9) from the thrust-reverser cowl hinge-fitting (2), you must use the 98D54003022000 RI BALL BEARING.
NOTE: The 98D54003022000 RI BALL BEARING has two sockets (5) and (6) and one screw puller (7).
   (2) Release the tabwasher (3) from the slotted nut (4).
   (3) Put the socket (5) on the outer ring (1) and hold them in position.
   (4) Put and hold the socket (6) on the slotted nut (4).
   (5) Remove and discard the slotted nut (4).
   (6) Remove and discard the tabwasher (3).
   (7) Remove the sockets (5) and (6).
   (8) Install the screw puller (7) on the thrust-reverser cowl hinge-fitting (2).
   (9) Tighten the screw puller (7) until the shim (8) touches the outer ring (1).
   (10) Tighten the screw puller (7) again to remove the outer ring (1) from the thrust-reverser cowl hinge-fitting (2).
   (11) Remove the outer ring (1) from the screw puller (7).
   (12) Discard the outer ring (1).
   (13) Remove the screw puller (7) from the thrust-reverser cowl hinge-fitting (2).
[Rev.10 from 2021] 2026.04.01 02:03:52 UTC