W DOC AIRBUS | AMM A320F

Installation of the Refuel Valve


TASK 28-25-51-400-001-A
Installation of the Refuel Valve


WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
FIN: 7QU
FIN: 8QU
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
SAFETY BARRIER(S)
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 0.80 and 0.70 m.daN (70.80 and 61.95 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.01ABA1)
Turbine Fuel-- Kerosene -
(Material No.03FAB1)
Mineral Oil base Grease-- Vaseline or Petrolatum -
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [7QU] (VALVE-REFUEL, L WING TK)
522JB
FOR [8QU] (VALVE-REFUEL, R WING TK)
622JB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
5
O-RING
AIPC 28-25-51-01-010
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 12-11-28-650-003-A
Pressure Refuel with Automatic Control
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
TASK 28-00-00-910-001-A
Fuel Safety Procedures
TASK 28-25-00-650-001-A
Pressure Defuel
TASK 28-25-00-869-001-A
Fuel Transfer
3. Job Set-up
Subtask 28-25-51-941-060-A
A. Safety Precautions
WARNING: OBEY THE FUEL SAFETY PROCEDURES.
   (1) You must obey the fuel safety procedures when you do work on the fuel system (Ref. AMM TASK 28-00-00-910-001).
   (2) Make sure that the SAFETY BARRIER(S) are in position.
   (3) Make sure that the WARNING NOTICE(S) is in position to tell persons not to operate the slat controls.
Subtask 28-25-51-860-051-A
B. Aircraft Maintenance Configuration
   (1) Make sure that the access platform is below the applicable access panel 522JB (622JB).
   (2) Make sure that the applicable access panel 522JB(622JB) is removed.
Subtask 28-25-51-865-056-A
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C NOT FOR ALL
121VUFUEL/RFL/DFL/SPLY2QUL24
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL23
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
** ON A/C NOT FOR ALL
121VUFUEL/RFL/DFL/SPLY2QUL23
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL22
4. Procedure
Subtask 28-25-51-420-054-A
A. Preparation for Installation
   (1) Clean the component interface and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (2) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (3) Do an inspection of the component interfaces and the adjacent area.
   (4) Lubricate the new AIPC 28-25-51-01-010 O-RING (5) and the internal surface of the valve canister with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
   (5) Install the O-ring (5) on the refuel valve (3).
Subtask 28-25-51-420-050-A
B. Installation of the Refuel Valve 7QU, (8QU)
   (1) Install the refuel valve (3) in the valve canister.
   (2) Install the nuts (2).
   (3) Torque the nuts (2) to between 0.80 and 0.70 m.daN (70.80 and 61.95 lbf.in ) T.
   (4) Use the screw (6) and nut (7) to attach the bonding strap (4) to the valve (3) (
Ref. AMM TASK 20-28-00-912-802).
   (5) Remove the blanking cap from the electrical connector (1).
   (6) Install the electrical connector (1).
Subtask 28-25-51-865-054-A
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUFUEL/RFL/DFL/SPLY2QUL24
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL23
** ON A/C NOT FOR ALL
121VUFUEL/RFL/DFL/SPLY2QUL23
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL22
Subtask 28-25-51-710-051-A
D. Test
   (1) To test the refuel valve:
   (2) Make sure there are no leaks from the refuel valve.
5. Close-up
Subtask 28-25-51-410-050-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the applicable access panel:

     (a) FOR [7QU] (VALVE-REFUEL, L WING TK)
install 522JB

     (b) FOR [8QU] (VALVE-REFUEL, R WING TK)
install 622JB.
Subtask 28-25-51-650-051-A
B. Fuel Configuration
   (1) Refuel, defuel or transfer fuel as necessary (Ref. AMM TASK 12-11-28-650-003), (Ref. AMM TASK 28-25-00-650-001) or (Ref. AMM TASK 28-25-00-869-001).
Subtask 28-25-51-865-058-A
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C NOT FOR ALL
121VUFUEL/RFL/DFL/SPLY2QUL24
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL23
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
** ON A/C NOT FOR ALL
121VUFUEL/RFL/DFL/SPLY2QUL23
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL22
Subtask 28-25-51-942-051-A
D. Removal of Equipment
   (1) Remove the safety barriers.
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.02 07:03:19 UTC