W DOC AIRBUS | AMM A320F

Removal of the Compressor Inlet Gasket


TASK 21-52-21-000-002-A
Removal of the Compressor Inlet Gasket


WARNING: MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE. HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
WARNING: BE CAREFUL WHEN YOU REMOVE OR INSTALL THIS EQUIPMENT. THIS EQUIPMENT IS HEAVY (MORE THAN 12 KG (26.5 lb)) AND CAN CAUSE INJURY AND/OR DAMAGE.
NOTE: This procedure is applicable for the air-cycle machine with part numbers 1263A0000-02/-03, 757A0000-08/-09/-10 and 1263C0000-01.
FIN: 10HM1
FIN: 11HM1
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
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [10HM1] (MACHINE-AIR CYCLE)
191KB
FOR [11HM1] (MACHINE-AIR CYCLE)
192KB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 21-52-21-000-001-A
Removal of the Air Cycle Machine
TASK 21-52-23-000-002-A
Removal of the Pipe Assembly between the Anti-Ice Valve (if installed), the Bypass Valve and the Air Cycle Machine
TASK 21-61-53-000-001-A
Removal of the Turbine Bypass Valve
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
3. Job Set-up
Subtask 21-52-21-861-053-A
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 21-52-21-865-055-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 10HM1 (MACHINEAIR CYCLE)
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
** ON A/C NOT FOR ALL
122VUAIR COND/PACK TEMP/CTL SYS1/1/115VAC1HHX22
122VUAIR COND/PACK TEMP/CTL SYS1/1/28VDC3HHX21
122VUAIR COND/PACK TEMP CTL SYS2/1/28VDC4HHY19
122VUAIR COND/PACK TEMP CTL SYS2/1/115VAC2HHY18
** ON A/C NOT FOR ALL
122VUAIR COND/TEMP CTL SYS 1/CHAN A/115VAC49HHX22
122VUAIR COND/TEMP CTL SYS 1/CHAN A/28VDC51HHX21
122VUAIR COND/TEMP CTL SYS 1/CHAN B/115VAC50HHY18
** ON A/C NOT FOR ALL
FOR FIN: 11HM1 (MACHINEAIR CYCLE)
122VUAIR COND/PACK TEMP/CTL SYS1/2/115VAC21HHW22
122VUAIR COND/PACK TEMP/CTL SYS1/2/28VDC23HHW21
122VUAIR COND/PACK TEMP CTL SYS2/2/28VDC24HHY21
122VUAIR COND/PACK TEMP CTL SYS2/2/115VAC22HHY20
** ON A/C NOT FOR ALL
122VUAIR COND/TEMP CTL SYS 2/CHAN A/115VAC53HHW22
122VUAIR COND/TEMP CTL SYS 2/CHAN A/28VDC55HHW21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/28VDC56HHY21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/115VAC54HHY20
Subtask 21-52-21-941-051-A
C. Safety Precautions
   (1) On AIR COND panel 30VU:
     (a) Make sure that:
  • The APU BLEED pushbutton switch is released (the ON legend is off)
  • The ENG 1 BLEED and the ENG 2 BLEED pushbutton switches are released (the OFF legends are on).
     (b) Put a WARNING NOTICE(S) in position to tell persons not to operate these pushbutton switches.
   (2) On the HP ground connector, put the WARNING NOTICE(S) in position to tell persons not to supply the ground air.
Subtask 21-52-21-010-052-A
D. Get Access
   (1) Remove these access panels from the belly fairing structure (Ref. AMM TASK 53-35-13-000-002):
     (a) FOR [10HM1] (MACHINE-AIR CYCLE)
     (b) FOR [11HM1] (MACHINE-AIR CYCLE)
   (2) Remove the clamp from the pipe assembly between the compressor inlet duct and the primary heat exchanger (Ref. AMM TASK 21-52-21-000-001).
   (3) If installed, remove the pipe assembly between the anti-ice valve, the bypass valve and the air cycle machine (Ref. AMM TASK 21-52-23-000-002).
   (4) Remove bypass valve 10HH (11HH) (Ref. AMM TASK 21-61-53-000-001).
4. Procedure
Subtask 21-52-21-020-053-A
A. Removal of the Compressor Inlet Gasket
CAUTION: WHEN YOU REMOVE THE SCREWS, MAKE SURE THAT YOU DO NOT CAUSE DAMAGE TO THE SCREWLOCKS. IF YOU CAUSE DAMAGE TO THE SCREWLOCKS, YOU MUST REMOVE THE UNIT AND SEND IT TO AN APPROVED REPAIR STATION.
   (1) For part number 1263A0000-02/-03:
     (a) Remove the screws (5) and the washers (4).
     (b) Remove the compressor inlet duct (3).
     (c) Remove and discard the compressor inlet gasket (2).
   (2) For part number 757A0000-08/-09/-10:
     (a) Remove the nuts (10) and the screws (6).
     (b) Remove the compressor inlet duct (9).
     (c) Remove and discard the packing (8).
   (3) For part number 1263C0000-01:
     (a) Remove the screws (5) and (7) and the washers (4) and (6).
     (b) Remove the compressor inlet duct (3).
     (c) Remove and discard the compressor inlet gasket (2).
[Rev.10 from 2021] 2026.04.02 06:11:27 UTC