W DOC AIRBUS | AMM A320F

Installation of the ACT Cabin Air Intake Check Valve


TASK 28-28-43-400-002-A
Installation of the ACT Cabin Air Intake Check Valve


WARNING: OBEY THE FUEL SAFETY PROCEDURES.
WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
WARNING: BE CAREFUL NOT TO GET AIRCRAFT FUEL IN YOUR MOUTH OR IN YOUR EYES. IF YOU GET FUEL ON YOUR SKIN OR ON YOUR CLOTHES, FLUSH IT IMMEDIATELY WITH WATER. IF NECESSARY, GET MEDICAL HELP. AIRCRAFT FUEL IS POISONOUS.
ZONE: 150
FIN: 179QM ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
150
AFT CARGO COMPARTMENT FWD PRESS BULKHEAD TO AFT BULKHEAD OF AFT CARGO COMPARTMENT
152DW, 826
 C. Referenced Information
REFERENCE
DESIGNATION
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 25-55-11-000-003-A
Removal of the Sidewall Panels in the Aft Cargo Compartment - FR47/FR59
TASK 25-55-11-400-003-A
Installation of the Sidewall Panels in the Aft Cargo Compartment - FR47/FR59
TASK 28-00-00-910-001-A
Fuel Safety Procedures
TASK 28-11-27-000-003-A
Removal of the Additional Center Tank No.2 (ACT AFT2)
TASK 28-11-27-400-003-A
Installation of the Additional Center Tank No.2 (ACT AFT2)
TASK 28-28-00-710-005-A
Operational Test of the Additional Center Tank (ACT) Automatic Transfer System
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 28-28-43-860-054-C ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
   (2) Make sure that the aircraft electrical circuits are energized.
(Ref. AMM TASK 24-41-00-861-002).
   (3) Make sure that the ACCESS PLATFORM 2M (6 FT) is below aft cargo compartment door 826.
   (4) Make sure that aft cargo compartment door 826 is open (Ref. AMM TASK 52-30-00-860-001).
   (5) Make sure that CARGO COMPT LIGHT switch 8LU is in the ON position.
   (6) Make sure that ACT AFT2 is removed from the aft cargo-compartment (Ref. AMM TASK 28-11-27-000-003).
   (7) On refuel/defuel control panels 801VU and 800VU, on fuel control panel 40VU and on Additional Center Tank (ACT) control panel 28VU:
     (a) Make sure that the WARNING NOTICE(S) is(are) in position to tell persons not to operate the refuel/defuel system.
   (8) Make sure that sidewall panel 152DW is removed (Ref. AMM TASK 25-55-11-000-003).
Subtask 28-28-43-865-054-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUFUEL/ACT AIR SOV/MAN/SPLY64QHJ20
121VUFUEL/ACT AIR SOV/AUTO/SPLY63QHJ19
121VUFUEL/ACT XFR VLV/MOT266QHJ18
121VUFUEL/ACT XFR VLV/MOT165QHJ17
121VUFUEL/HI/LVL/SPLY1QJL24
121VUFUEL/RFL/DFL/SPLY2QUL23
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL22
121VUFUEL/ACT VENT VLV/MAN/SPLY62QHL21
121VUFUEL/ACT VENT VLV/AUTO/SPLY61QHL20
121VUFUEL/ACT/FUEL PUMP/SPLY25QHQ29
4. Procedure
Subtask 28-28-43-420-051-B ** ON A/C NOT FOR ALL
A. Installation of the Check Valve
   (1) Remove the PLUG-BLANKING from each disconnected line end.
   (2) Clean the component interfaces and the adjacent area.
   (3) Do an inspection of the component interfaces and the adjacent area.
CAUTION: USE A SECOND WRENCH TO HOLD THE FITTINGS WHEN YOU LOOSEN/TIGHTEN THE TUBE COUPLING NUTS. THIS PREVENTS DAMAGE TO THE TUBES.
   (4) Connect the pipe (2) to the check valve (3) and tighten the union nut (1).
   (5) Connect the pipe (5) to the check valve (3) and tighten the union nut (4).
Subtask 28-28-43-865-055-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUFUEL/ACT AIR SOV/MAN/SPLY64QHJ20
121VUFUEL/ACT AIR SOV/AUTO/SPLY63QHJ19
121VUFUEL/ACT XFR VLV/MOT266QHJ18
121VUFUEL/ACT XFR VLV/MOT165QHJ17
121VUFUEL/HI/LVL/SPLY1QJL24
121VUFUEL/RFL/DFL/SPLY2QUL23
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL22
121VUFUEL/ACT VENT VLV/MAN/SPLY62QHL21
121VUFUEL/ACT VENT VLV/AUTO/SPLY61QHL20
121VUFUEL/ACT/FUEL PUMP/SPLY25QHQ29
Subtask 28-28-43-710-051-A ** ON A/C NOT FOR ALL
C. Test(s)
   (1) Do the operational test of the ACT automatic transfer system (Ref. AMM TASK 28-28-00-710-005).
5. Close-up
Subtask 28-28-43-410-051-C ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) In the aft cargo-compartment, install the sidewall panel 152DW (Ref. AMM TASK 25-55-11-400-003).
   (3) In the aft cargo-compartment, install ACT AFT2 (Ref. AMM TASK 28-11-27-400-003).
   (4) Set CARGO COMPT LIGHT switch 8LU to the OFF position.
   (5) Remove the access platforms(s).
   (6) Close aft cargo-compartment door 826 (Ref. AMM TASK 52-30-00-860-002).
Subtask 28-28-43-860-055-A ** ON A/C NOT FOR ALL
B. Put the aircraft back to the serviceable condition.
   (1) From refuel/defuel control panels 801VU and 800VU, on fuel control panel 40VU and on Additional Center Tank (ACT) control panel 28VU:
     (a) Remove the WARNING NOTICE(S).
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:17:58 UTC