W DOC AIRBUS | AMM A320F

Installation of the Lavatory and Galley Extract Fan


TASK 21-23-51-400-001-A
Installation of the Lavatory and Galley Extract Fan


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.
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 0.18 and 0.13 m.daN (15.93 and 11.50 lbf.in ) T
No specific
Torque wrench: range to between 0.25 and 0.2 m.daN (22.12 and 17.70 lbf.in ) T
No specific
Torque wrench: range to between 0.30 and 0.25 m.daN (26.55 and 22.12 lbf.in ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
162DW, 826
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
TASK 21-61-00-710-001-A
Operational Test of the Pack Temperature-Control System
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 25-55-12-000-001-A
Removal of the Aft Cargo-Compartment Partition at FR65
TASK 25-55-12-400-001-A
Installation of the Aft Cargo-Compartment Partition at FR65
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
3. Job Set-up
Subtask 21-23-51-860-050-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) The AFT cargo-compartment door 826 is open (Ref. AMM TASK 52-30-00-860-001).
     (c) The ACCESS PLATFORM 2M (6 FT) is in position at the AFT cargo-compartment door 826.
     (d) The access panel 162DW is removed (Ref. AMM TASK 25-55-12-000-001).
Subtask 21-23-51-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
122VUAIR COND/LAV/GALLEY VENT CTL/EXTRACT FAN/CTL5HUU21
122VUAIR COND/LAV/GALLEY VENT CTL/EXTRACT FAN/SPLY6HUU19
4. Procedure
Subtask 21-23-51-420-050-B
A. Installation of the Lavatory and Galley Extract Fan
   (1) Remove the blanking plugs from the lavatory and galley extract fan (3) and from the duct (11).
   (2) Put the lavatory and galley extract fan (3) in position on the duct (11) and in the bracket (13).
NOTE: Make sure that the flow arrow on the body of the lavatory and galley extract fan (3) points in the direction of the air flow.
   (3) Install the clamps (2) and (4).
NOTE: Make sure that when you look in the direction of the air flow the electrical connector on the lavatory and galley extract fan is between the 4 o'clock and the 5 o'clock position.
   (4) Make sure that the clamp (4) is in the correct position.
   (5) TORQUE the clamp (4) to between 0.30 and 0.25 m.daN (26.55 and 22.12 lbf.in ) T.
   (6) Make sure that the clamp (2) is in the correct position.
   (7) TORQUE the clamp (2) to between 0.18 and 0.13 m.daN (15.93 and 11.50 lbf.in )
T.
   (8) Put the outlet duct (12) in position on the lavatory and galley extract fan (3) and install the clamp (1).
NOTE: Make sure that the location pin (14) is engaged in the hole in the lavatory and galley extract fan outlet-flange.
   (9) Make sure that the clamp (1) is in the correct position.
   (10) TORQUE the clamp (1) to between 0.25 and 0.2 m.daN (22.12 and 17.70 lbf.in )
T.
   (11) Put the bonding strap (8) in position and install the washer (9), the screw (10), the washer (7) and the nut (6) (
Ref. AMM TASK 20-28-00-912-802).
   (12) Remove the blanking caps from the disconnected electrical connectors.
   (13) Make sure that all the electrical connections are clean and in the correct condition.
   (14) Connect the electrical connector (5).
   (15) Make sure that the work area is clean and clear of tools and other items.
Subtask 21-23-51-865-052-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
122VUAIR COND/LAV/GALLEY VENT CTL/EXTRACT FAN/CTL5HUU21
122VUAIR COND/LAV/GALLEY VENT CTL/EXTRACT FAN/SPLY6HUU19
Subtask 21-23-51-710-050-A
C. Do the operational test of the pack temperature-control system (Ref. AMM TASK 21-61-00-710-001)
5. Close-up
Subtask 21-23-51-410-050-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 162DW (Ref. AMM TASK 25-55-12-400-001).
   (3) Remove the access platform.
   (4) Close the AFT cargo-compartment door 826 (Ref. AMM TASK 52-30-00-860-002).
Subtask 21-23-51-862-050-A
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:10:56 UTC