W DOC AIRBUS | AMM A320F

Operational Check of LP Shut Off Valves and Their Controls to Ensure No Flow When Selected Closed With Booster Pump On

TASK 28-24-00-790-003-A
Operational Check of LP Shut Off Valves and Their Controls to Ensure No Flow When Selected Closed With Booster Pump On

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
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.
ZONE: 210
ZONE: 430
ZONE: 440
ZONE: 520
ZONE: 620
FIN: 12QM
FIN: 13QM
1. Reason for the Job
Refer to the MPD TASK: 282400-01
OPERATIONAL CHECK OF LP SHUT OFF VALVES AND THEIR CONTROLS TO ENSURE NO FLOW WHEN SELECTED CLOSED WITH BOOSTER PUMP ON
NOTE: Two person are necessary to do this task. One person to operate the fuel pumps from the cockpit and one person to monitor the fuel flow.
NOTE: You can also do this task during the engine removal before the task interval.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
AR
CONTAINER - CLEAN, APPLICABLE
No specific
AR
CONTAINER 200 L (53 USGAL)
No specific
AR
CONTAINER 20L (5 USGAL)
No specific
AR
CONTAINER 4 L (1 USGAL)
No specific
1
PLUG - BLANKING
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 0.62 and 0.51 m.daN (54.87 and 45.13 lbf.in ) T
No specific
Torque wrench: range to between 1.13 and 1.02 m.daN (100.00 and 90.27 lbf.in ) T
No specific
Torque wrench: range to between 1.36 and 1.24 m.daN (120.35 and 109.73 lbf.in ) T
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP5070)
vaseline
(Material No.CP8001)
lockwire 0.032 in. (0.8 mm) dia.
(Material No.CP8002)
lockwire 0.032 in. (0.8 mm) dia
(Material No.CP8006)
safety cable 0.032 in. (0.8 mm) dia.
(Material No.P03-001)
lubricant, aircraft turbine engine
(Material No.V02-147)
lockwire
(Material No.V10-077)
lubricant (engine oil)
(Material No.01ABA1)
Turbine Fuel-- Kerosene -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
210
CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD
430
ENG 1 AIR INTAKE, FAN AND ACCESS GEARBOX
440
ENG 2 AIR INTAKE, FAN AND ACCESS GEARBOX
520
LEFT WING FIXED LEADING EDGE
620
RIGHT WING FIXED LEADING EDGE
522AT, 622AT
FOR [12QM] (VALVE-LP FUEL, ENG 1)
522AT
FOR [13QM] (VALVE-LP FUEL, ENG 2)
622AT
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
PACKING
EIPC 73-11-02-01-280
2
PACKING
AIPC 73-11-10-01-147
2
PACKING
AIPC 73-11-10-01-290
1
PACKING
AIPC 73-12-42-80-070
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 12-11-28-650-003-A
Pressure Refuel with Automatic Control
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 28-24-00-710-803-A
Operational Check of LP Shut Off Valves including Operation by Individual Motors
TASK 31-60-00-860-001-A
EIS Start Procedure
TASK 31-60-00-860-002-A
EIS Stop Procedure
TASK 70-23-11-911-013-A
General Torque Tightening Techniques
TASK 70-23-13-911-010-A
Procedures for the Installation of Preformed Packings
TASK 71-13-00-010-010-A
Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
TASK 71-13-00-010-802-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-010-A
Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-040-A
Closing of the Fan Cowl Doors
TASK 71-13-00-410-040-B
Closing of the Fan Cowl Doors
TASK 71-13-00-410-802-A
Closing of the Fan Cowl Doors
TASK 73-11-11-000-040-A
Removal of the Main Fuel Supply Hose
TASK 73-11-11-000-041-A
Removal of the Main Fuel Supply Hose
TASK 73-11-11-400-040-A
Installation of the Main Fuel Supply Hose
TASK 73-11-11-400-041-A
Installation of the Main Fuel Supply Hose
TASK 73-11-48-000-010-A
Removal of the Power Plant Flexible Fuel Tubes
TASK 73-11-48-000-802-A
Removal of the Main Fuel Line
TASK 73-11-48-400-010-A
Installation of the Power Plant Flexible Fuel Tubes
TASK 73-11-48-400-802-A
Installation of the Main Fuel Line
F Component Location - Cockpit ** ON A/C NOT FOR ALL
F Component Location - Cockpit ** ON A/C NOT FOR ALL
F Component Location - Cockpit ** ON A/C NOT FOR ALL
F Component Location - Cockpit ** ON A/C NOT FOR ALL
F Component Location - Cockpit ** ON A/C NOT FOR ALL
F Component Location - Cockpit ** ON A/C NOT FOR ALL
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
FOR [12QM] (VALVE-LP FUEL, ENG 1)
TASK 57-41-37-000-003-A
Removal of the Access Panel
TASK 57-41-37-400-003-A
Installation of the Access Panel
FOR [13QM] (VALVE-LP FUEL, ENG 2)
TASK 57-41-37-000-003-A
Removal of the Access Panel
TASK 57-41-37-400-003-A
Installation of the Access Panel
3. Job Set-up
Subtask 28-24-00-941-057-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) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 28-24-00-860-056-A
B. Aircraft Maintenance Configuration
   (1) Make sure each wing fuel tank contains a minimum of 1000 kg (2205 lb) of fuel. Refuel if necessary (Ref. AMM TASK 12-11-28-650-003).
   (2) On overhead panel 20VU, make sure that the ENG 1 and ENG 2 FIRE pushbutton switches (P/BSW) are in the closed and guarded position.
   (3) On engine panel 115VU, make sure that the ENG/MASTER 1 and ENG/MASTER 2 switches are in the OFF position.
   (4) Make sure that there is a WARNING NOTICE(S) on overhead panel 20VU, to tell persons not to operate the ENG 1 and ENG 2 FIRE pushbutton switches.
   (5) Make sure that there is a WARNING NOTICE(S) on engine panel 115VU, to tell persons not to operate the ENG/MASTER 1 and 2 switches.
   (6) On flaps panel 114VU:
     (a) Install a 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever.
     (b) Put a WARNING NOTICE(S) in position on the flap/slat control lever to tell persons not to operate the flap/slat controls.
   (7) On the SD FUEL page, make sure that the crossfeed valve indication shows green cross-line (valve closed).
Subtask 28-24-00-010-054-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position adjacent to the applicable pylon.
   (2) Open the engine fan-cowl doors (Ref. AMM TASK 71-13-00-010-040).
   (3) Remove these access panels:
     (a) FOR [12QM] (VALVE-LP FUEL, ENG 1)
522AT (Ref. AMM TASK 57-41-37-000-003).
     (b) FOR [13QM] (VALVE-LP FUEL, ENG 2)
622AT (Ref. AMM TASK 57-41-37-000-003).
   (4) Keep the slats in the deployed position.
Subtask 28-24-00-010-054-B ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position adjacent to the applicable pylon.
   (2) Open the engine fan-cowl doors (Ref. AMM TASK 71-13-00-010-010).
   (3) Remove these access panels:
     (a) FOR [12QM] (VALVE-LP FUEL, ENG 1)
522AT (Ref. AMM TASK 57-41-37-000-003).
     (b) FOR [13QM] (VALVE-LP FUEL, ENG 2)
622AT (Ref. AMM TASK 57-41-37-000-003).
   (4) Keep the slats in the deployed position.
Subtask 28-24-00-010-054-E ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position adjacent to the applicable pylon.
   (2) Open the engine fan-cowl doors (Ref. AMM TASK 71-13-00-010-802).
   (3) Remove these access panels:
     (a) FOR [12QM] (VALVE-LP FUEL, ENG 1)
522AT (Ref. AMM TASK 57-41-37-000-003).
     (b) FOR [13QM] (VALVE-LP FUEL, ENG 2)
622AT (Ref. AMM TASK 57-41-37-000-003).
   (4) Keep the slats in the deployed position.
4. Procedure
WARNING: WHEN YOU OPERATE THE FUEL PUMPS DURING A MAINTENANCE PROCEDURE, A MAINTENANCE PERSON MUST BE IN THE COCKPIT. THIS PERSON MUST STOP THE PUMPS WHEN THE LOW PRESSURE FAULT LIGHT(S) (ON PANEL 40VU) COME ON, TO PREVENT OPERATION OF THE PUMPS(S) WITHOUT FUEL ('DRY RUNNING'). OPERATION OF THE PUMPS WITHOUT FUEL CAN CAUSE A FIRE.
Subtask 28-24-00-710-059-A
A. Operational Test
   (1) Do an operational check of the applicable LP shut-off valves (Ref. AMM TASK 28-24-00-710-803):
     (a) Make sure that access panels 522AT ( 622AT) are not installed after this procedure.
Subtask 28-24-00-860-057-A
B. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
   (3) In the cockpit, on ECAM control-panel 11VU:
     (a) Push the FUEL pushbutton switch to get the FUEL system page on the ECAM lower display-unit.
Subtask 28-24-00-865-064-A
C. Open, safety and tag 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 ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 28-24-00-865-065-A
D. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUFUEL/LP VALVE/MOT1/ENG22QGA09
49VUFUEL/LP VALVE/MOT1/ENG11QGA08
121VUFUEL/LP VALVE/MOT2/ENG24QGM26
121VUFUEL/LP VALVE/MOT2/ENG13QGM25
Subtask 28-24-00-680-050-B ** ON A/C NOT FOR ALL
E. Drain the remaining fuel from the engine and the pylon fuel hose at the fuel filter as follows:
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Put a CONTAINER - CLEAN, APPLICABLE under the fuel filter.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
   (2) Cut, remove and discard the lockwire from the fuel drain plug (2).
   (3) Remove the fuel drain plug (2) from the fuel filter.
   (4) Remove and discard the packing (1) from the fuel drain plug (2).
   (5) Drain the fuel into the container.
NOTE: Do not put fuel that you drained from the engine back into the fuel system.
Subtask 28-24-00-860-058-B ** ON A/C NOT FOR ALL
F. Aircraft Maintenance Configuration
   (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (2) Put a WARNING NOTICE(S) in position to tell persons not to energize the aircraft electrical circuits.
   (3) Put a CONTAINER - CLEAN, APPLICABLE below the fuel feed-line to collect fuel spillage.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU DO WORK ON OR NEAR THE FUEL SYSTEM. THE FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY.
   (4) Disconnect the main fuel feed-line at:
   (5) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 28-24-00-680-050-C ** ON A/C NOT FOR ALL
G. Drain the remaining fuel from the engine and the pylon fuel hose at the fuel filter as follows:
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Put a CONTAINER 4 L (1 USGAL) under the fuel filter.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
   (2) Cut, remove and discard the lockwire from the fuel drain plug (1).
   (3) Remove the fuel drain plug (1) from the fuel filter.
   (4) Remove and discard the packing (2) from the fuel drain plug (1).
   (5) Drain the fuel into the container.
NOTE: Do not put fuel that you drained from the engine back into the fuel system.
Subtask 28-24-00-860-058-A ** ON A/C NOT FOR ALL
H. Aircraft Maintenance Configuration
   (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (2) Put a WARNING NOTICE(S) in position to tell persons not to energize the aircraft electrical circuits.
   (3) Put a CONTAINER - CLEAN, APPLICABLE below the fuel feed-line to collect fuel spillage.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU DO WORK ON OR NEAR THE FUEL SYSTEM. THE FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY.
   (4) Disconnect the main fuel feed-line at: Disconnect the main fuel feed-line at:
   (5) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 28-24-00-680-050-D ** ON A/C NOT FOR ALL
I. Drain the remaining fuel from the engine and the pylon fuel hose at the fuel filter as follows:
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Put a CONTAINER 4 L (1 USGAL) under the fuel filter.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
   (2) Cut, remove and discard the lockwire or safety cable from the fuel drain plug (1).
   (3) Remove the fuel drain plug (1) from the fuel filter.
   (4) Remove and discard the packing (2) from the fuel drain plug (1).
   (5) Drain the fuel into the container.
NOTE: Do not put fuel that you drained from the engine back into the fuel system.
Subtask 28-24-00-860-058-C ** ON A/C NOT FOR ALL
J. Aircraft Maintenance Configuration
   (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (2) Put a WARNING NOTICE(S) in position to tell persons not to energize the aircraft electrical circuits.
   (3) Put a CONTAINER - CLEAN, APPLICABLE below the fuel feed-line to collect fuel spillage.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU DO WORK ON OR NEAR THE FUEL SYSTEM. THE FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY.
   (4) Disconnect the main fuel feed-line at:
   (5) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 28-24-00-680-050-E ** ON A/C NOT FOR ALL
K. Drain the remaining fuel from the engine and the pylon fuel hose at the fuel manifold as follows:
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Put a CONTAINER 20L (5 USGAL) in position below the fuel manifold.
   (2) Loosen the drain plug bolt (3), turn and remove the fuel drain plug (1).
   (3) Remove and discard the packing (2) from the fuel drain plug (1).
   (4) Drain the fuel into the CONTAINER 20L (5 USGAL).
     (a) Make sure that you do not put fuel that you drained from the engine back into the fuel system.
Subtask 28-24-00-860-058-F ** ON A/C NOT FOR ALL
L. Aircraft Maintenance Configuration
   (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (2) Put a WARNING NOTICE(S) in position to tell persons not to energize the aircraft electrical circuits.
   (3) Put a CONTAINER - CLEAN, APPLICABLE below the fuel feed-line to collect fuel spillage.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU DO WORK ON OR NEAR THE FUEL SYSTEM. THE FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY.
   (4) Disconnect the main fuel feed-line at:
   (5) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 28-24-00-790-054-A ** ON A/C NOT FOR ALL
M. Do this test for each LP valve 12QM(13QM)
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
   (1) Do the steps that follow:
ACTION
RESULT
1.On the ECAM lower display-unit:

  • Make sure that the LP valve is in the closed position (cross-line).
2.On fuel panel 40VU:

  • Push (in) L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switch.
On fuel panel 40VU:

  • The OFF lights go off
  • The FAULT lights come on momentarily.


The fuel feed-line to the LP valve is pressurized.
3.Keep the fuel feed line pressurized for three minutes, then examine these parts for fuel leakage:

  • The main fuel feed-line (3)
  • The LP valve externally.

    Make sure that there are no leaks.
4.On fuel panel 40VU:

  • Release (out) L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switch.
On fuel panel 40VU:

  • L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switch OFF lights come on.
   (2) If you find a fuel leakage, repair the leak:
  • Do this test again.
Subtask 28-24-00-790-054-B ** ON A/C NOT FOR ALL
M. Do this test for each LP valve 12QM(13QM)
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
   (1) Do the steps that follow:
ACTION
RESULT
1.On the ECAM lower display-unit:

  • Make sure that the LP valve is in the closed position (cross-line).
2.On fuel panel 40VU:

  • Push (in) L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switch.
On fuel panel 40VU:

  • The OFF lights go off
  • The FAULT lights come on momentarily.


The fuel feed-line to the LP valve is pressurized.
3.Keep the fuel feed line pressurized for three minutes, then examine these parts for fuel leakage:

  • The main fuel feed-line (1) at the fluid disconnect panel
  • The LP valve externally.

    Make sure that there are no leaks.
4.On fuel panel 40VU:

  • Release (out) L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switches.
On fuel panel 40VU:

  • L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switch OFF lights come on.
   (2) If you find a fuel leakage, repair the leak:
  • Do this test again.
Subtask 28-24-00-790-054-C ** ON A/C NOT FOR ALL
M. Do this test for each LP valve 12QM(13QM)
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
   (1) Do the steps that follow:
ACTION
RESULT
1.On the ECAM lower display-unit:

  • Make sure that the LP valve is in the closed position (cross-line).
2.On fuel panel 40VU:

  • Push (in) L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switches.
On fuel panel 40VU:

  • The OFF lights go off
  • The FAULT lights come on momentarily.


The fuel feed-line to the LP valve is pressurized.
3.Keep the fuel feed line pressurized for three minutes, then examine these parts for fuel leakage:

  • The main fuel feed-line (5)
  • The LP valve externally.

    Make sure that there are no leaks.
4.On fuel panel 40VU:

  • Release (out) L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switches.
On fuel panel 40VU:

  • L TK PUMPS 1 and 2 (R TK PUMPS 1 and 2) pushbutton switch OFF lights come on.
   (2) If you find a fuel leakage, repair the leak:
  • Do this test again.
Subtask 28-24-00-860-059-A ** ON A/C NOT FOR ALL
N. Aircraft Maintenance Configuration
   (1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (3) Connect the disconnected end of the main fuel-feed line (Ref. AMM TASK 73-11-11-400-040).
   (4) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (5) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
Subtask 28-24-00-860-059-B ** ON A/C NOT FOR ALL
N. Aircraft Maintenance Configuration
   (1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (3) Connect the disconnected end of the main fuel-feed line (Ref. AMM TASK 73-11-48-400-010).
   (4) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (5) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
Subtask 28-24-00-860-059-C ** ON A/C NOT FOR ALL
N. Aircraft Maintenance Configuration
   (1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (3) Connect the disconnected end of the main fuel-feed line (Ref. AMM TASK 73-11-11-400-041).
   (4) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (5) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
Subtask 28-24-00-860-059-F ** ON A/C NOT FOR ALL
N. Aircraft Maintenance Configuration
   (1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (3) Connect the disconnected end of the main fuel-feed line (Ref. AMM TASK 73-11-48-400-802).
   (4) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (5) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
Subtask 28-24-00-020-052-A
O. Put a CONTAINER 200 L (53 USGAL) in position below the fuel filter.

F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Do a check of the fuel flow during the test:
     (a) Make sure that you do not put fuel that you drained from the engine back into the fuel system.
Subtask 28-24-00-420-054-B ** ON A/C NOT FOR ALL
P. Installation of Fuel Drain-Plug 12QM (13QM)

F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Install the fuel drain plug (1) on the fuel manifold as follows:
     (a) Apply P03-001lubricant, aircraft turbine engine to the new EIPC 73-11-02-01-280 PACKING (2).
     (b) Install the packing (2) on the fuel drain plug (1).
     (c) Install and turn the fuel drain plug (1) below the washer (4) and the drain plug bolt (3).
     (d) TORQUE the drain plug bolt (3) to between 1.13 and 1.02 m.daN (100.00 and 90.27 lbf.in ) T
Subtask 28-24-00-420-054-D ** ON A/C NOT FOR ALL
P. Installation of Fuel Drain-Plug 12QM (13QM)

F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Install the fuel drain plug (2) on the fuel filter as follows:
     (a) Lubricate a new AIPC 73-12-42-80-070 PACKING (1) with clean V10-077lubricant (engine oil) (Ref. AMM TASK 70-23-13-911-010).
     (b) Install the packing (1) on the fuel drain plug (2).
     (c) Install the fuel drain plug (2) on the fuel filter.
     (d) TORQUE the fuel drain plug (2) to between 1.36 and 1.24 m.daN (120.35 and 109.73 lbf.in ) T (Ref. AMM TASK 70-23-11-911-013).
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
     (e) Safety the fuel drain plug with the lockwire (Material No.V02-147) .
Subtask 28-24-00-420-054-E ** ON A/C NOT FOR ALL
P. Installation of Fuel Drain-Plug 12QM (13QM)

F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Install the fuel drain plug (1) on the fuel filter as follows:
     (a) Soak the new AIPC 73-11-10-01-147 PACKING (2) in Turbine Fuel-- Kerosene - (Material No.01ABA1) .
     (b) Lubricate the packing (2) with vaseline (Material No.CP5070) .
     (c) Install the packing (2) on the fuel drain plug (1).
     (d) Install the fuel drain plug (1) on the fuel filter.
     (e) TORQUE the fuel drain plug (1) to between 0.62 and 0.51 m.daN (54.87 and 45.13 lbf.in ) T.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
     (f) Safety the fuel drain plug (1) with the CP8001lockwire 0.032 in. (0.8 mm) dia. or with the CP8006safety cable 0.032 in. (0.8 mm) dia..
Subtask 28-24-00-420-054-F ** ON A/C NOT FOR ALL
P. Installation of Fuel Drain-Plug 12QM (13QM)

F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
   (1) Install the fuel drain plug (1) on the fuel filter as follows:
     (a) Soak the new AIPC 73-11-10-01-290 PACKING (2) in Turbine Fuel-- Kerosene - (Material No.01ABA1) .
     (b) Lubricate the packing (2) with vaseline (Material No.CP5070) .
     (c) Install the packing (2) on the fuel drain plug (1).
     (d) Install the fuel drain plug (1) on the fuel filter.
     (e) TORQUE the fuel drain plug (1) to between 0.62 and 0.51 m.daN (54.87 and 45.13 lbf.in ) T.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
     (f) Safety the fuel drain plug (1) with the CP8001lockwire 0.032 in. (0.8 mm) dia. or with the CP8002lockwire 0.032 in. (0.8 mm) dia.
Subtask 28-24-00-420-055-B
DELETED
Subtask 28-24-00-420-055-D
DELETED
Subtask 28-24-00-420-055-E
DELETED
Subtask 28-24-00-420-055-F
DELETED
5. Close-up
Subtask 28-24-00-860-083-A
A. Aircraft Maintenance Configuration
   (1) On ECAM CP 11VU, push (in) the FUEL P/BSW to get the FUEL system page on the ECAM lower DU.
   (2) On panel 115VU, put the applicable ENG/MASTER 1 or ENG/MASTER 2 switch to the ON position.
   (3) On the ECAM lower DU, make sure that the applicable LEFT or RIGHT LP valve is open (green in-line).
Subtask 28-24-00-865-077-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUFUEL/LP VALVE/MOT1/ENG22QGA09
49VUFUEL/LP VALVE/MOT1/ENG11QGA08
121VUFUEL/LP VALVE/MOT2/ENG24QGM26
121VUFUEL/LP VALVE/MOT2/ENG13QGM25
Subtask 28-24-00-860-071-A
C. Aircraft Maintenance Configuration (continued)
   (1) On panel 115VU:
  • Put the applicable ENG/MASTER 1 or ENG/MASTER 2 switches in the OFF position.
   (2) On panel 40VU:
  • Push (in) the applicable L TK PUMPS 1 and 2 or R TK PUMPS 1 and 2 P/BSW
  • Make sure that the P/BSW OFF lights go off and the P/BSW FAULT lights come on momentarily.
Subtask 28-24-00-790-055-A ** ON A/C NOT FOR ALL
D. Leak Test
   (1) Examine the flange of the main fuel feed-line (1) connection for fuel leakage. Fuel leakage from the main fuel feed-line (1) connection is not permitted.
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
   (2) Examine the fuel drain plug (1) for fuel leakage. Fuel leakage from the fuel drain plug (1) is not permitted.
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
Subtask 28-24-00-790-055-B ** ON A/C NOT FOR ALL
D. Leak Test
   (1) Examine the flange of the main fuel feed-line (3) connection for fuel leakage. Fuel leakage from the main fuel feed-line (3) connection is not permitted.
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
   (2) Examine the fuel drain plug (2) for fuel leakage. Fuel leakage from the fuel drain plug (2) is not permitted.
F Fuel Drain Plug - Location and Detail ** ON A/C NOT FOR ALL
Subtask 28-24-00-860-072-A
E. Aircraft Maintenance Configuration
   (1) On panel 40VU:
  • Release (out) the L TK PUMPS 1 and 2 or R TK PUMPS 1 and 2 P/BSW
  • Make sure that the P/BSW OFF lights come on.
Subtask 28-24-00-865-087-A
F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUFUEL/LP VALVE/MOT1/ENG22QGA09
49VUFUEL/LP VALVE/MOT1/ENG11QGA08
121VUFUEL/LP VALVE/MOT2/ENG24QGM26
121VUFUEL/LP VALVE/MOT2/ENG13QGM25
Subtask 28-24-00-860-070-A
G. Aircraft Maintenance Configuration
   (1) On the ECAM DU, make sure that the LP valves are closed.
   (2) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
   (3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 28-24-00-410-055-A ** ON A/C NOT FOR ALL
H. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install these access panels:
     (a) FOR [12QM] (VALVE-LP FUEL, ENG 1)
522AT (Ref. AMM TASK 57-41-37-400-003).
     (b) FOR [13QM] (VALVE-LP FUEL, ENG 2)
622AT (Ref. AMM TASK 57-41-37-400-003).
   (3) Close the engine fan-cowl doors (Ref. AMM TASK 71-13-00-410-040).
Subtask 28-24-00-420-050-A ** ON A/C NOT FOR ALL
I. If the engine is not installed
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
   (1) Install a PLUG - BLANKING on the main fuel feed-line (3).
Subtask 28-24-00-410-055-B ** ON A/C NOT FOR ALL
J. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install these access panels:
     (a) FOR [12QM] (VALVE-LP FUEL, ENG 1)
522AT (Ref. AMM TASK 57-41-37-400-003).
     (b) FOR [13QM] (VALVE-LP FUEL, ENG 2)
622AT (Ref. AMM TASK 57-41-37-400-003).
   (3) Close the engine fan-cowl doors (Ref. AMM TASK 71-13-00-410-010).
Subtask 28-24-00-420-050-B ** ON A/C NOT FOR ALL
K. If the engine is not installed
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
   (1) Install a PLUG - BLANKING on the main fuel feed-line (1).
Subtask 28-24-00-410-055-E ** ON A/C NOT FOR ALL
L. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install these access panels:

     (a) FOR [12QM] (VALVE-LP FUEL, ENG 1)
522AT (Ref. AMM TASK 57-41-37-400-003).
     (b) FOR [13QM] (VALVE-LP FUEL, ENG 2)
622AT (Ref. AMM TASK 57-41-37-400-003).
   (3) Close the engine fan-cowl doors (Ref. AMM TASK 71-13-00-410-802).
Subtask 28-24-00-420-050-C ** ON A/C NOT FOR ALL
M. If the engine is not installed
F Main Fuel Feed Line - Location and Detail ** ON A/C NOT FOR ALL
   (1) Install a PLUG - BLANKING on the main fuel feed-line (5).
Subtask 28-24-00-865-067-A
N. 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 ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 28-24-00-942-057-A
O. Removal of Equipment
   (1) Remove the SAFETY BARRIERS.
   (2) Remove the fuel container.
   (3) Remove the access platform(s).
   (4) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap/slat control lever.
   (5) Remove the WARNING NOTICE(S).
   (6) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.02 06:17:34 UTC
"WTRUIB" 2025