W DOC AIRBUS | AMM A320F

Installation of the Cabin Recirculation Fans


TASK 21-21-51-400-001-A
Installation of the Cabin Recirculation Fans


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 the cabin recirculation fans 15HG and 14HG.
FIN: 14HG
FIN: 15HG
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT)
No specific
Torque wrench: range to between 1.120 and 0.916 m.daN (99.12 and 81.06 lbf.in ) T
No specific
Torque wrench: range to between 1.32 and 1.08 m.daN (116.81 and 95.58 lbf.in ) T
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
TASK 21-21-00-710-001-A
Operational Test of the Cabin Recirculation Fans
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 25-54-12-000-001-A
Removal of the Forward Cargo-Compartment Partition
TASK 25-54-12-400-001-A
Installation of the Forward Cargo-Compartment Partition
TASK 52-30-00-860-001-A
Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
TASK 52-30-00-860-002-A
Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
FOR [14HG] (RECIRC FAN 2)
TASK 06-41-53-00
FUSELAGE-DESCRIPTION AND OPERATION
FOR [15HG] (RECIRC FAN 1)
TASK 06-41-53-00
FUSELAGE-DESCRIPTION AND OPERATION
3. Job Set-up
Subtask 21-21-51-860-050-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) On the panel 30VU:
       1 The APU BLEED pushbutton switch is in the off position (the ON legend is off).
       2 The ENG 1 BLEED and the ENG 2 BLEED pushbutton switches are in the off position (the OFF legends are on).
       3 The warning notice to tell persons not to operate these pushbutton switches is in position.
     (c) On the HP and the LP ground connector the warning notice to tell persons not to supply the ground air is in position.
     (d) The FWD cargo-compartment door 865 is open (Ref. AMM TASK 52-30-00-860-001).
     (e) The ACCESS PLATFORM 2M (6 FT) is in position at the FWD cargo-compartment door 865.
     (f) The access panels at partition FR34 are removed (Ref. AMM TASK 25-54-12-000-001).
     (g) FOR [15HG] (RECIRC FAN 1)
     (h) FOR [14HG] (RECIRC FAN 2)
Subtask 21-21-51-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
FOR FIN: 15HG (RECIRC FAN 1)
122VUAIR COND/RECIRC FAN/L/CTL2HGX20
122VUAIR COND/RECIRC FAN/L/SPLY1HGX18
FOR FIN: 14HG (RECIRC FAN 2)
122VUAIR COND/RECIRC FAN/R/CTL11HGW20
122VUAIR COND/RECIRC FAN/R/SPLY3HGW18
4. Procedure
Subtask 21-21-51-420-050-A
A. Installation of the Cabin Recirculation Fan
   (1) Remove the blanking plugs from the cabin recirculation fan (15), the sleeve (1) and from the check valve (7). .
NOTE: Make sure that the check valve (7) is installed and that it is in the correct position.
The center line of the hinge must be in a vertical position.
   (2) Make sure that the sleeve (1) is clean and free from obstructions.
   (3) Clean the component interfaces and the adjacent area.
   (4) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (5) Put the recirculation fan lugs (16) in position and install the washers (4), the bolts (3), the washers (5) and the nuts (6).
   (6) TORQUE the nuts (6) to between 1.32 and 1.08 m.daN (116.81 and 95.58 lbf.in ) T.
   (7) Put the clamp (13) in position.
     (a) TORQUE the clamp (13) to between 1.120 and 0.916 m.daN (99.12 and 81.06 lbf.in )
T.
   (8) Put the clamp (2) and the sleeve (1) in position on the cabin recirculation fan (15).
NOTE: The end of the sleeve (1) must be within the coloured markings painted on the cabin recirculation fan (15).
   (9) Tighten the clamp (2).
   (10) Put the bonding strap (10) in position and install the washer (9), the bolt (8), the washer (11) and the nut (12) (
Ref. AMM TASK 20-28-00-912-802).
   (11) Remove the blanking plugs from the disconnected electrical connectors.
   (12) Make sure that all the electrical connections are clean and in the correct condition.
   (13) Connect the electrical connector (14).
   (14) Make sure that the work area is clean and clear of tools and other items.
Subtask 21-21-51-710-050-A
B. Do the operational test of the cabin recirculation fans 14HG (15HG). (Ref. AMM TASK 21-21-00-710-001)
5. Close-up
Subtask 21-21-51-410-050-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 at partition FR34 (Ref. AMM TASK 25-54-12-400-001).
     (a) FOR [15HG] (RECIRC FAN 1)
     (b) FOR [14HG] (RECIRC FAN 2)
   (3) Remove the access platform(s).
   (4) Close the FWD cargo-compartment door 865 (Ref. AMM TASK 52-30-00-860-002).
   (5) Remove the WARNING NOTICE(S).
Subtask 21-21-51-865-052-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
FOR FIN: 15HG (RECIRC FAN 1)
122VUAIR COND/RECIRC FAN/L/CTL2HGX20
122VUAIR COND/RECIRC FAN/L/SPLY1HGX18
FOR FIN: 14HG (RECIRC FAN 2)
122VUAIR COND/RECIRC FAN/R/CTL11HGW20
122VUAIR COND/RECIRC FAN/R/SPLY3HGW18
Subtask 21-21-51-862-050-A
C. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002)
[Rev.10 from 2021] 2026.04.02 06:47:30 UTC