W DOC AIRBUS | AMM A320F

Installation of the Pipe Assembly between the Anti-Ice Valve (if installed), the Bypass Valve and the Air Cycle Machine


TASK 21-52-23-400-002-A
Installation of the Pipe Assembly between the Anti-Ice Valve (if installed), the Bypass Valve and the Air Cycle Machine


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 USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
NOTE: The procedure for the removal of the pipe assembly is the same for the left and right side.
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
Torque wrench: range to between 0.55 and 0.50 m.daN (48.67 and 44.25 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03QBB9)
Dry lubricant-General Assembly Molybdenum Disulfide -
(Material No.03QBD1)
Dry lubricant-General Assembly Graphite -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [10HM] (PACK 1-AIR CONDITIONING)
191KB
FOR [11HM] (PACK 2-AIR CONDITIONING)
192KB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
PACKING
AIPC 21-52-41-27-020
4
SEAL
AIPC 21-52-41-27-035
6
SEAL
AIPC 21-52-41-27-035
3
PACKING
AIPC 21-52-41-27-055
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 12-33-21-618-001-A-01
Pre-conditioning through the HP Ground Connection
TASK 12-33-21-618-001-A-02
Pre-conditioning with the APU
TASK 20-26-00-910-002-A
Installation of Expansion Joints
TASK 21-52-00-200-002-A
Detailed Visual Inspection of the Pipe Assemblies between the Heat Exchanger Unit, the Bypass Valve, the Anti-Ice Valve (if installed) and the Air Cycle Machine
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 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
TASK 53-35-13-400-002-A
Installation of the Quick-Release Access Panels on the Belly Fairing Structure
F Pipe Assembly. ** ON A/C NOT FOR ALL
F Pipe Assembly ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 21-52-23-860-052-A
A. Aircraft Maintenance Configuration
   (1) Make sure that:
     (a) The aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
     (b) The access panel is removed (Ref. AMM TASK 53-35-13-000-002),
       1 FOR [10HM] (PACK 1-AIR CONDITIONING)
       2 FOR [11HM] (PACK 2-AIR CONDITIONING)
     (c) On the overhead panel, on AIR COND panel 30VU:
       1 The APU BLEED pushbutton switch is released (the ON legend is off).
       2 The ENG 1 BLEED and the ENG 2 BLEED pushbutton switches are released (the OFF legends are on).
       3 The warning notice is in position to tell persons not to operate these pushbutton switches.
     (d) On the HP ground connector, the warning notice is in position to tell persons not to supply ground air.
Subtask 21-52-23-865-055-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 10HM (PACK 1AIR CONDITIONING)
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: 11HM (PACK 2AIR CONDITIONING)
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
4. Procedure
Subtask 21-52-23-210-053-A
A. Inspection of the Pipe Assembly
   (1) Do the visual inspection of the pipe assembly (Ref. AMM TASK 21-52-00-200-002).
Subtask 21-52-23-560-051-A ** ON A/C NOT FOR ALL
B. Preparation of the Replacement Component (if necessary)
   (1) Disconnect the clamp (5) from the removed pipe assembly (8).
   (2) Remove the blanking plate (4).
   (3) Remove and discard the packing (3).
   (4) Put a new AIPC 21-52-41-27-055 PACKING (3) in position on the replacement pipe assembly (8).
   (5) Put the blanking plate (4) in position on the pipe assembly (8).
   (6) Install the clamp (5).
   (7) TORQUE the clamp (5) to between 0.55 and 0.50 m.daN (48.67 and 44.25 lbf.in )
T.
Subtask 21-52-23-420-050-C ** ON A/C NOT FOR ALL
C. Installation of the Pipe Assembly
   (1) Do the visual inspection of the pipe assembly (
Ref. AMM TASK 21-52-00-200-002).
   (2) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (3) Apply lubricant:
CAUTION: USE ONLY THE SPECIFIED LUBRICANT TO LUBRICATE THE O-RINGS AND THE PACKINGS. OTHER LUBRICANTS CAN CAUSE SMOKE OR A SMELL IN THE CABIN WHEN THEY BECOME HOT.
     (a) Apply a small quantity of:
       1 The material 03QBB9 is a molybdenum disulfide powder. Before you apply it, mix the powder with pure water or white spirit and make it into a paste.
       2 Apply the material 03QBD1 dry.
   (4) Remove the PLUG-BLANKING from each disconnected line end.
   (5) Clean the component interfaces and the adjacent area.
   (6) Put the new
AIPC 21-52-41-27-035 SEAL (4) in position in the pipe assembly (8) (Ref. AMM TASK 20-26-00-910-002).
   (7) Put the packing (2) in position on the air-cycle machine (1) and the packing (3) in position on the pipe assembly (8).
   (8) Carefully put the pipe assembly (8) in position on the by-pass valve (7), the air-cycle machine (1) and the anti-ice valve (6).
   (9) Install the clamps (5) and (9).
   (10) Make sure that the clamps (5) and (9) are in the correct position.
   (11) TORQUE the clamps (5) and (9) to between 0.55 and 0.50 m.daN (48.67 and 44.25 lbf.in ) T.
   (12) Make sure that the work area is clean and clear of tools and other items.
Subtask 21-52-23-420-050-D ** ON A/C NOT FOR ALL Subtask 21-52-23-865-066-A
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 10HM (PACK 1AIR CONDITIONING)
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: 11HM (PACK 2AIR CONDITIONING)
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 21-52-23-710-051-A
E. Test
   (1) Do the pre-conditioning through the HP ground connector (
Ref. AMM TASK 12-33-21-618-001) or with the APU (Ref. AMM TASK 12-33-21-618-001).
   (2) Do a leak check of the pipe assembly connections.
Make sure that there are no leaks.
   (3) After approximately 15 minutes stop the pre-conditioning (Ref. AMM TASK 12-33-21-618-001) or (Ref. AMM TASK 12-33-21-618-001).
5. Close-up
Subtask 21-52-23-410-057-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the access panel (Ref. AMM TASK 53-35-13-400-002):
     (a) FOR [10HM] (PACK 1-AIR CONDITIONING)
     (b) FOR [11HM] (PACK 2-AIR CONDITIONING)
   (3) Remove the WARNING NOTICE(S).
Subtask 21-52-23-862-051-A
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:48:35 UTC