DOC AIRBUS | AMM A320FInstallation of the LP Fuel Valve Actuator
TASK 28-24-51-400-001-A
Installation of the LP Fuel Valve Actuator
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 28-24-51-941-053-A
Subtask 28-24-51-420-051-A
Subtask 28-24-51-410-050-A
[Rev.10 from 2021]
2026.04.02 06:17:35 UTC
Installation of the LP Fuel Valve Actuator
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
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.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.03FAB1) | Mineral Oil base Grease-- Vaseline or Petrolatum - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [10QG] (ACTUATOR-LP FUEL VALVE, ENG 2) | |
| 622AT | |
| FOR [9QG] (ACTUATOR-LP FUEL VALVE, ENG 1) | |
| 522AT | |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 4 | O-RING | AIPC 28-24-41-01-010 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-11-28-650-003-A | Pressure Refuel with Automatic Control |
| TASK 27-80-00-866-004-A | Extending the Slats on the Ground |
| TASK 28-00-00-200-002-A | Dimensional Inspection of the Dowel (Anti-Rotation) on Twin Motor Actuators |
| TASK 28-00-00-910-001-A | Fuel Safety Procedures |
| TASK 28-24-00-720-001-A | Functional Test of the LP Fuel Shut Off Valves |
| TASK 28-25-00-650-001-A | Pressure Defuel |
| TASK 28-25-00-869-001-A | Fuel Transfer |
| TASK 57-41-37-000-003-A | Removal of the Access Panel |
| TASK 57-41-37-400-003-A | Installation of the Access Panel |
LP Fuel Valve Actuator - LH WingSubtask 28-24-51-941-053-A
A. Safety Precautions
(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 slats.
Subtask 28-24-51-860-052-A 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 slats.
B. Aircraft Maintenance Configuration
(1) Make sure that the slats are fully extended (Ref. AMM TASK 27-80-00-866-004).
(2) Make sure that the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE is below the applicable access panel 522AT(622AT).
(3) Make sure that the applicable access panel 522AT(622AT) is removed (Ref. AMM TASK 57-41-37-000-003).
(4) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is on the slat/flap control lever.
Subtask 28-24-51-865-052-A (1) Make sure that the slats are fully extended (Ref. AMM TASK 27-80-00-866-004).
(2) Make sure that the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE is below the applicable access panel 522AT(622AT).
(3) Make sure that the applicable access panel 522AT(622AT) is removed (Ref. AMM TASK 57-41-37-000-003).
(4) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is on the slat/flap control lever.
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 9QG (ACTUATORLP FUEL VALVE, ENG 1) | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C ALL | |||
| 49VU | FUEL/LP VALVE/MOT1/ENG1 | 1QG | A08 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 121VU | FUEL/LP VALVE/MOT2/ENG1 | 3QG | M25 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 10QG (ACTUATORLP FUEL VALVE, ENG 2) | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C ALL | |||
| 49VU | FUEL/LP VALVE/MOT1/ENG2 | 2QG | A09 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 121VU | FUEL/LP VALVE/MOT2/ENG2 | 4QG | M26 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
Subtask 28-24-51-420-051-A
A. Preparation for Installation
(3) Do a visual inspection of the component interface and/or the adjacent area.
(4) Make sure that the parts retained from the removed component are clean and in the correct condition.
(5) Carefully align the drive spindle (6) of the drive assembly (turn, if necessary) with the drive key (8) of the actuator (2).
(6) Make sure that the roll pin is aligned to its related locating hole in the actuator (2).
Subtask 28-24-51-420-050-A CAUTION:
DO NOT TRY TO TURN THE DRIVE OF THE ACTUATOR BECAUSE YOU WILL CAUSE DAMAGE.
(1) Do the dimensional check of the dowel (anti-rotation) for the actuator with the part numbers that follow (Ref. AMM TASK 28-00-00-200-002): - HTE190001
- HTE190001-1
- HTE190001-2.
(3) Do a visual inspection of the component interface and/or the adjacent area.
(4) Make sure that the parts retained from the removed component are clean and in the correct condition.
(5) Carefully align the drive spindle (6) of the drive assembly (turn, if necessary) with the drive key (8) of the actuator (2).
(6) Make sure that the roll pin is aligned to its related locating hole in the actuator (2).
B. Installation of the LP Fuel Valve Actuator
(2) Install the new O-ring (4) on the drive assembly of the LP fuel valve (5).
(3) Make sure that the actuator (2) and the drive spindle (6) stay in the correct configuration.
(4) Carefully install the actuator (2) on the drive assembly of the LP fuel valve (5).
(a) Make sure that the mating surfaces of the actuator (2) and of the drive assembly touch fully with:
.
(6) Make sure that the V-clamp (3) is fully engaged.
(8) Connect the electrical connectors (1) to the actuator (2).
Subtask 28-24-51-865-054-A CAUTION:
MAKE SURE THAT YOU CORRECTLY ALIGN THE POSITIONS OF THE ROLL PIN ON THE DRIVE SPINDLE AND THE PIN HOLE IN THE ACTUATOR. IF NOT, THE ACTUATOR WILL NOT OPERATE THE VALVE CORRECTLY AND CAN CAUSE FUEL LEAKAGE.
CAUTION:
DO NOT TORQUE THE V-CLAMP(S) TO MORE THAN THE SPECIFIED VALUE. THIS PREVENTS DAMAGE TO THE FLANGE SURFACES.
(1) Lubricate the new AIPC 28-24-41-01-010 O-RING (4) with Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) . (2) Install the new O-ring (4) on the drive assembly of the LP fuel valve (5).
(3) Make sure that the actuator (2) and the drive spindle (6) stay in the correct configuration.
(4) Carefully install the actuator (2) on the drive assembly of the LP fuel valve (5).
(a) Make sure that the mating surfaces of the actuator (2) and of the drive assembly touch fully with:
- the drive key of the actuator spindle engaged with the spindle of the drive assembly
- the roll pin in the drive assembly engaged with the locating hole in the actuator (2)
- the dowel in the flange of the actuator engaged with the slot of the drive assembly.
- actuator (2)
- drive assembly.
NOTE: There will always be no clearance when the pins and the grooves are all correctly aligned.
(5) Install the V-clamp (3) and TORQUE the screw (7) to between 0.143 and 0.117 m.daN (12.65 and 10.35 lbf.in ) . (6) Make sure that the V-clamp (3) is fully engaged.
NOTE: The V-clamp (3) is fully engaged if no part of the flange shows for the:
(7) Remove the blanking caps from the electrical connectors (1). - actuator (2)
- drive assembly.
(8) Connect the electrical connectors (1) to the actuator (2).
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 28-24-51-720-051-A 5. Close-up| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 9QG (ACTUATORLP FUEL VALVE, ENG 1) | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C ALL | |||
| 49VU | FUEL/LP VALVE/MOT1/ENG1 | 1QG | A08 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 121VU | FUEL/LP VALVE/MOT2/ENG1 | 3QG | M25 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 10QG (ACTUATORLP FUEL VALVE, ENG 2) | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C ALL | |||
| 49VU | FUEL/LP VALVE/MOT1/ENG2 | 2QG | A09 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 121VU | FUEL/LP VALVE/MOT2/ENG2 | 4QG | M26 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
Subtask 28-24-51-410-050-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 522AT(622AT) (Ref. AMM TASK 57-41-37-400-003):
(a) FOR [9QG] (ACTUATOR-LP FUEL VALVE, ENG 1)
panel 522AT.
(b) FOR [10QG] (ACTUATOR-LP FUEL VALVE, ENG 2)
panel 622AT.
Subtask 28-24-51-860-053-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access panel 522AT(622AT) (Ref. AMM TASK 57-41-37-400-003):
(a) FOR [9QG] (ACTUATOR-LP FUEL VALVE, ENG 1)
panel 522AT.
(b) FOR [10QG] (ACTUATOR-LP FUEL VALVE, ENG 2)
panel 622AT.
B. Aircraft Maintenance Configuration
(1) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the slat/flap control lever.
(2) Fully retract the slats (Ref. AMM TASK 27-80-00-866-004).
(3) 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 28-24-51-942-051-A (1) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the slat/flap control lever.
(2) Fully retract the slats (Ref. AMM TASK 27-80-00-866-004).
(3) 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).
C. 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.
(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.