W DOC AIRBUS | AMM A320F

Replacement of the Upper Seals of the Bleed-Air Precooler Exchanger


TASK 54-52-22-300-801-B
Replacement of the Upper Seals of the Bleed-Air Precooler Exchanger


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.
ZONE: 410
ZONE: 420
1. Reason for the Job
Refer to the MPD TASK: 361101-01
DISCARD PRE COOLER EXCHANGER (PCE) UPPER SEAL.
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)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
410
ENG 1 PYLON BOX AND FORWARD FAIRING
420
ENG 2 PYLON BOX AND FORWARD FAIRING
413DT, 423DT
 C. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
3
SEALS
AIPC 54-52-81-33-050
2
SEALS
AIPC 54-52-81-33-060
3
SEALS
AIPC 54-52-81-34-050
2
SEALS
AIPC 54-52-81-34-060
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 54-52-11-000-807-A
Removal of the Access Skin Panels
TASK 54-52-11-400-807-A
Installation of the Access Skin Panels
TASK 78-30-00-040-807-A
Deactivation of the Thrust Reverser System for Nacelle Maintenance (ICU)
TASK 78-30-00-440-807-A
Reactivation of the Thrust Reverser System after Nacelle Maintenance (ICU)
3. Job Set-up
Subtask 54-52-22-941-053-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 was in the OFF position not less than five minutes before you do this procedure.
     (c) Put a 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 a WARNING NOTICE(S) in position to tell persons not to energize FADEC 1(2).
Subtask 54-52-22-040-052-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 thrust reverser unserviceable for maintenance (Ref. AMM TASK 78-30-00-040-807).
Subtask 54-52-22-010-052-A
C. Get Access
   (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position:
     (a) For the left pylon, in zone 410
     (b) For the right pylon, in zone 420.
   (2) Remove the access skin panels (Ref. AMM TASK 54-52-11-000-807):
     (a) For the left pylon: 413DT
     (b) For the right pylon: 423DT.
4. Procedure
Subtask 54-52-22-300-053-A 5. Close-up
Subtask 54-52-22-410-052-A
A. Close Access
   (1) Install the access skin panels (
Ref. AMM TASK 54-52-11-400-807):
     (a) For the left pylon: 413DT
     (b) For the right pylon: 423DT.
Subtask 54-52-22-440-052-A
B. Reactivation of the Thrust Reverser
   (1) Make the thrust reverser serviceable after maintenance (Ref. AMM TASK 78-30-00-440-807).
Subtask 54-52-22-942-052-A
C. Aircraft Maintenance Configuration
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 02:02:10 UTC