W DOC AIRBUS | AMM A320F

Installation of the Primary Heat Exchanger


TASK 21-52-25-400-001-A
Installation of the Primary Heat Exchanger


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.
FIN: 10HM6
FIN: 11HM6
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 0.45 and 0.4 m.daN (39.82 and 35.40 lbf.in ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [10HM6] (HEAT EXCHANGER-PRIMARY)
191KB
FOR [11HM6] (HEAT EXCHANGER-PRIMARY)
192KB
 C. 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 21-52-24-400-001-A
Installation of the Heat Exchanger Unit (into the Aircraft)
TASK 21-52-24-400-001-A-01
Installation of the Heat Exchanger Unit (Into the Air Conditioning Pack)
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
3. Job Set-up
Subtask 21-52-25-865-051-A
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 10HM6 (HEAT EXCHANGERPRIMARY)
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: 11HM6 (HEAT EXCHANGERPRIMARY)
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 21-52-25-860-050-A
B. Aircraft Maintenance Configuration
   (1) Make sure that the access panel/s is/are removed (Ref. AMM TASK 53-35-13-000-002).
     (a) FOR [10HM6] (HEAT EXCHANGER-PRIMARY)
     (b) FOR [11HM6] (HEAT EXCHANGER-PRIMARY)
4. Procedure
Subtask 21-52-25-420-050-A
A. Installation of the Primary Heat Exchanger
NOTE: It is not necessary to install the gaskets (4) and (6) during the installation of the primary heat exchanger.
   (1) Remove the protective covers from the cooling elements of the primary heat exchanger (5) and the main heat exchanger (9).
   (2) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (3) Clean the component interfaces and the adjacent area.
   (4) Put the primary heat exchanger (5) in position on the main heat exchanger (9) and install the washers (7) and the screws (8).
   (5) TORQUE the screws (8) to between 0.45 and 0.4 m.daN (39.82 and 35.40 lbf.in ) T.
   (6) Put the fan plenum (1) in position on the primary heat exchanger (5) and install the washers (3) and the screws (2).
   (7) TORQUE the screws (2) to between 0.45 and 0.4 m.daN (39.82 and 35.40 lbf.in )
T.
   (8) Install the heat exchanger unit (
Ref. AMM TASK 21-52-24-400-001).
Subtask 21-52-25-865-052-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: 10HM6 (HEAT EXCHANGERPRIMARY)
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: 11HM6 (HEAT EXCHANGERPRIMARY)
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 21-52-25-710-050-A
C. Test
   (1) Do the pre-conditioning through the HP ground connector or with the APU (Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
   (2) Do a leak check of the primary heat exchanger connections.
NOTE: Minimum leakage is permitted. After the pack operates some minutes, the leakage of air will reduce because the seals have their correct operating temperature.
   (3) After approx. 15 minutes stop the pre-conditioning (Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
5. Close-up
Subtask 21-52-25-410-050-A
A. Close Access
   (1) Install the access panel/s (Ref. AMM TASK 53-35-13-400-002).
     (a) FOR [10HM6] (HEAT EXCHANGER-PRIMARY)
     (b) FOR [11HM6] (HEAT EXCHANGER-PRIMARY)
Subtask 21-52-25-862-050-A
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:47:32 UTC