W DOC AIRBUS | AMM A320F

Removal of the Additional Center Tank (ACT) Fuel Inlet-Valve-Actuator


TASK 28-28-54-000-003-A
Removal of the Additional Center Tank (ACT) Fuel Inlet-Valve-Actuator


WARNING: OBEY THE FUEL SAFETY PROCEDURES.
ZONE: 150
ZONE: 160
FIN: 94QH1 ** ON A/C NOT FOR ALL
FIN: 94QH2 ** 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
1
ACCESS PLATFORM 2M (6 FT)
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
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
160
BULK CARGO COMPARTMENT AFT BULKHEAD OF AFT CARGO COMPARTMENT TO AFT BULKHEAD OF BULK CARGO COMPARTMENT
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 28-00-00-910-001-A
Fuel Safety Procedures
TASK 52-30-00-860-001-A
Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
FOR [94QH1] (ACTUATOR-FUEL INLET VALVE, ACT1)
TASK 28-11-27-000-003-A
Removal of the Additional Center Tank No.2 (ACT AFT2)
FOR [94QH2] (ACTUATOR-FUEL INLET VALVE, ACT2)
TASK 28-11-49-000-002-A
Removal of the Additional Center Tank (ACT) Integrated Impact Wall
3. Job Set-up
Subtask 28-28-54-860-054-A ** 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) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (3) On refuel/defuel control panels 801VU and 800VU, fuel control panel 40VU and ACT control panel 28VU:
     (a) Put the WARNING NOTICE(S) to tell persons not to operate the refuel/defuel system.
Subtask 28-28-54-865-054-A ** ON A/C NOT FOR ALL
B. Open, safety and tag 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/INLET VLV MOT2 AUTO SP AFT 244QH2K16
121VUFUEL/INLET VLV MOT2 AUTO SP AFT 144QH1K15
121VUFUEL/INLET VLV/MOT1/AFT 284QHL29
121VUFUEL/INLET VLV/MOT1/MAN SPLY/AFT 146QHL28
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/INLET VLV MAN CTL SPLY AFT 281QHL16
121VUFUEL/INLET VLV MAN CTL SPLY AFT 145QHL15
121VUFUEL/ACT/FUEL PUMP/SPLY25QHQ29
Subtask 28-28-54-010-053-D ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put an ACCESS PLATFORM 2M (6 FT) in position below aft cargo compartment door 826.
   (2) Open aft cargo compartment door 826 (Ref. AMM TASK 52-30-00-860-001).
   (3) Set CARGO COMPT LIGHT switch 8LU to the ON position.
   (4) FOR [94QH1] (ACTUATOR-FUEL INLET VALVE, ACT1)
     (a) Remove the Additional Center Tank (ACT) AFT2 (Ref. AMM TASK 28-11-27-000-003).
   (5) FOR [94QH2] (ACTUATOR-FUEL INLET VALVE, ACT2)
     (a) Remove the integrated impact wall from the ACT AFT2 (Ref. AMM TASK 28-11-49-000-002).
4. Procedure
Subtask 28-28-54-020-052-A ** ON A/C NOT FOR ALL
A. Removal of the ACT Fuel Inlet-Valve-Actuator
NOTE: The removal procedure is the same for each fuel inlet valve-actuator.
   (1) Disconnect the electrical connectors:
CAUTION: TO PREVENT POSSIBLE CROSS-CONNECTION OF THE ELECTRICAL CONNECTORS, MAKE SURE THAT PLUGS AND RECEPTACLES ARE CLEARLY IDENTIFIED.
CAUTION: MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
     (a) Put the identification marks on the electrical connectors (5) and receptacles (6) before you disconnect them. This is important for the subsequent installation procedure.
CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE COMPONENT DURING THE PROCEDURE. IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO COMPONENT.
     (b) Disconnect the electrical connectors (5) from the receptacles (6).
     (c) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
   (2) Loosen the screw (3), then open and remove the V-clamp (2) from the ACT fuel inlet-valve-actuator (1).
   (3) Remove the ACT fuel inlet-valve-actuator (1) from the ACT fuel inlet valve (4).
[Rev.10 from 2021] 2026.04.02 06:18:00 UTC