W DOC AIRBUS | AMM A320F

Installation of the Additional Center Tank (ACT) Water Drain-Valve


TASK 28-11-47-400-003-A
Installation of the Additional Center Tank (ACT) Water Drain-Valve


WARNING: OBEY THE FUEL SAFETY PROCEDURES.
WARNING: BEFORE YOU DO WORK IN OR NEAR A FUEL TANK, MAKE SURE THAT YOU OBEY ALL THE SAFETY PROCEDURES. THIS WILL PREVENT INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
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.
WARNING: DO NOT GET YOUR CLOTHES SOAKED WITH FUEL.
WARNING: MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT AVAILABLE.
ZONE: 150
ZONE: 160
FIN: 226QM1 ** ON A/C NOT FOR ALL
FIN: 226QM2 ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
150
AFT CARGO COMPARTMENT FWD PRESS BULKHEAD TO AFT BULKHEAD OF AFT CARGO COMPARTMENT
160
BULK CARGO COMPARTMENT AFT BULKHEAD OF AFT CARGO COMPARTMENT TO AFT BULKHEAD OF BULK CARGO COMPARTMENT
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 12-11-28-650-003-A
Pressure Refuel with Automatic Control
TASK 12-11-28-650-004-A
Pressure Refuel with Manual Control
TASK 12-11-28-650-005-A
Pressure Refuel without Electrical Power
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 28-00-00-910-001-A
Fuel Safety Procedures
TASK 28-25-00-650-005-A
To Drain the Remaining Fuel from the Additional Center Tank (ACT)
FOR [226QM1] (VALVE-WATER DRAIN, ACT1)
TASK 28-11-27-000-002-A
Removal of Additional Center Tank No.1 (ACT AFT1)
TASK 28-11-27-400-002-A
Installation of Additional Center Tank No.1 (ACT AFT1)
FOR [226QM2] (VALVE-WATER DRAIN, ACT2)
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)
3. Job Set-up
Subtask 28-11-47-860-059-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 ACT is completely drained from fuel (Ref. AMM TASK 28-25-00-650-005).
   (4) FOR [226QM2] (VALVE-WATER DRAIN, ACT2)
     (a) Make sure that ACT AFT2 is removed (Ref. AMM TASK 28-11-27-000-003).
   (5) FOR [226QM1] (VALVE-WATER DRAIN, ACT1)
     (a) Make sure that ACT AFT1 is removed (Ref. AMM TASK 28-11-27-000-002).
   (6) On refuel/defuel control panels 801VU and 800VU and on fuel control panel 40VU:
     (a) Make sure that the WARNING NOTICE(S) are in position to tell persons not to operate the refuel/defuel system.
4. Procedure
Subtask 28-11-47-420-053-C ** ON A/C NOT FOR ALL
A. Installation of the ACT Water Drain-Valve
CAUTION: DO THIS PROCEDURE ONLY IN THE WORKSHOP. IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE BLADDER TANK CAN OCCUR.
   (1) Install the water drain valves in ACT AFT1 and/or ACT AFT2.
Subtask 28-11-47-410-059-C ** ON A/C NOT FOR ALL
B. Close Access
   (1) FOR [226QM1] (VALVE-WATER DRAIN, ACT1)
     (a) Install ACT AFT1 (Ref. AMM TASK 28-11-27-400-002).
   (2) FOR [226QM2] (VALVE-WATER DRAIN, ACT2)
     (a) Install ACT AFT2 (Ref. AMM TASK 28-11-27-400-003).
Subtask 28-11-47-790-052-A ** ON A/C NOT FOR ALL
C. Leak Test
NOTE: The procedure for each ACT is the same.
   (1) Refuel the ACT (Ref. AMM TASK 12-11-28-650-003) (Ref. AMM TASK 12-11-28-650-004) (Ref. AMM TASK 12-11-28-650-005).
   (2) Examine the connection between the ACT water drain-valve and the ACT for leaks.
NOTE: Leaks are not permitted.
5. Close-up
Subtask 28-11-47-860-060-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to the serviceable condition.
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) From refuel/defuel control panels 801VU and 800VU, fuel control panel 40VU and from ACT control panel 28VU:
     (a) Remove the WARNING NOTICE(S).
   (3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:17:06 UTC