W DOC AIRBUS | AMM A320F

Replacement of the Hose

TASK 21-52-32-960-801-A
Replacement of the Hose

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.
NOTE: The procedure is the same for condensers 10HM2 and 11HM2.
ZONE: 191
ZONE: 192
1. Reason for the Job
NOTE: The procedure is only applicable when the hose is installed.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
Torque wrench: range to between 0.1 and 0.05 m.daN (8.85 and 4.42 lbf.in ) T
No specific
Torque wrench: range to between 0.28 and 0.26 m.daN (24.78 and 23.01 lbf.in ) T
No specific
Torque wrench: range to between 0.67 and 0.55 m.daN (59.29 and 48.67 lbf.in ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
191
AIR CONDITIONING COMPT AND FAIRINGS
192
AIR CONDITIONING COMPT AND FAIRINGS
FOR [10HM2] (CONDENSER)
191BB, 191KB
FOR [11HM2] (CONDENSER)
192FB, 192KB
 C. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
HOSE
AIPC 21-52-32-02-010
4
CLAMP
AIPC 21-52-32-02-020
5
SCREW
AIPC 21-52-32-02-040
6
WASHER
AIPC 21-52-32-02-050
 D. 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 21-63-00-710-004-A
Operational Test of the Cockpit and Cabin Temperature Control with CFDS/MCDU
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 Hose
3. Job Set-up
Subtask 21-52-32-861-052-A
A. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 21-52-32-865-054-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 10HM2 (CONDENSER)
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: 11HM2 (CONDENSER)
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 21-52-32-010-051-A
C. Get Access
   (1) Remove the access panel(s) (Ref. AMM TASK 53-35-13-000-002):
     (a) FOR [10HM2] (CONDENSER)
     (b) FOR [11HM2] (CONDENSER)
4. Procedure
Subtask 21-52-32-960-050-A
A. Replacement of the Hose
F Hose
   (1) Remove the screw (5) and the washer (6).
   (2) Loosen the clamps (4).
   (3) Remove the hose (2) from the condenser (1).
   (4) Remove the clamps (8) and (4) from the hose (2).
   (5) If damaged, remove and discard the AIPC 21-52-32-02-020 CLAMP (4), the AIPC 21-52-32-02-040 SCREW (5) and the AIPC 21-52-32-02-050 WASHER (6).
   (6) Put the new AIPC 21-52-32-02-010 HOSE (2) in position on the inlet tubes (3) of the condenser (1).
   (7) Install the clamps (4) on the new hose (2).
   (8) TORQUE the clamps (4):
   (9) Put the clamp (8) in position on the hose (2).
   (10) Install the washer (6) and the screw (5) on the bracket (7).
   (11) TORQUE the screw (5) to between 0.67 and 0.55 m.daN (59.29 and 48.67 lbf.in ) T.
Subtask 21-52-32-865-055-A
B. 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: 10HM2 (CONDENSER)
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: 11HM2 (CONDENSER)
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 21-52-32-710-051-A
C. 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 condenser connections.
NOTE: Minimum leakage is permitted. After the pack operates for some minutes, the leakage of air will decrease because the seals have their correct operating temperature.
   (3) Do a leak check of the sense line connections:
     (a) Make sure that there are no leaks.
   (4) 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) Do the operational test of the cockpit and cabin temperature control (Ref. AMM TASK 21-63-00-710-004).
5. Close-up
Subtask 21-52-32-410-052-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(s) (Ref. AMM TASK 53-35-13-400-002):
     (a) FOR [10HM2] (CONDENSER)
     (b) FOR [11HM2] (CONDENSER)
   (3) Remove the WARNING NOTICE(S).
Subtask 21-52-32-862-051-A
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:11:30 UTC
"WTRUIB" 2025