Visual Check of Pipes, Couplings and LP Valve External to Tank From Front Spar to Disconnect Panel For Leaks With Booster Pump On and LP Valve Open
TASK 28-21-00-790-002-A
Visual Check of Pipes, Couplings and LP Valve External to Tank From Front Spar to Disconnect Panel For Leaks With Booster Pump On and LP Valve Open
Refer to the MPD TASK: 282100-05
VISUAL CHECK OF PIPES, COUPLINGS AND LP VALVE EXTERNAL TO TANK FROM FRONT SPAR TO DISCONNECT PANEL FOR LEAKS WITH BOOSTER PUMP ON AND LP VALVE OPEN
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 28-21-00-790-053-A ** ON A/C NOT FOR ALL
Subtask 28-21-00-860-078-A
[Rev.10 from 2021]
2026.04.01 00:04:11 UTC
Visual Check of Pipes, Couplings and LP Valve External to Tank From Front Spar to Disconnect Panel For Leaks With Booster Pump On and LP Valve Open
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Refer to the MPD TASK: 282100-05
VISUAL CHECK OF PIPES, COUPLINGS AND LP VALVE EXTERNAL TO TANK FROM FRONT SPAR TO DISCONNECT PANEL FOR LEAKS WITH BOOSTER PUMP ON AND LP VALVE OPEN
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 2M (6 FT) |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 410 | ENG 1 PYLON BOX AND FORWARD FAIRING |
| 420 | ENG 2 PYLON BOX AND FORWARD FAIRING |
| 520 | LEFT WING FIXED LEADING EDGE |
| 620 | RIGHT WING FIXED LEADING EDGE |
| 437AL, 447AL, 452AR, 462AR | |
| 413ET, 423ET, 424DR, 452DR, 452ER, 462DR, 462ER | |
| 413AL, 413CL, 414AZ, 423AL, 423AZ, 423CL, 471AL, 481AL | |
| 413EL, 414FR, 423FL, 424ER | |
| 423CR, 471AR, 471BL, 471BR, 481AR, 481BL, 481BR | |
| 472AR, 482AR |
| 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 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TASK 54-52-11-000-002-A | Removal of the Access Panels |
| TASK 54-52-11-000-002-B | Removal of the Access Panels |
| TASK 54-52-11-400-002-A | Installation of the Access Panels |
| TASK 54-52-11-400-002-B | Installation of the Access Panels |
| TASK 54-53-11-000-002-A | Removal of the Pylon-to-Wing Access Panels |
| TASK 54-53-11-000-002-B | Removal of the Pylon-to-Wing Access Panels |
| TASK 54-53-11-000-804-A | Removal of the Pylon-to-Wing Access Panels and Doors |
| TASK 54-53-11-400-002-A | Installation of the Pylon-to-Wing Access Panels |
| TASK 54-53-11-400-002-B | Installation of the Pylon-to-Wing Access Panels |
| TASK 54-53-11-400-804-A | Installation of the Pylon-to-Wing Access Panels and Doors |
| 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 78-32-00-010-010-A | Opening of the Thrust Reverser Halves |
| TASK 78-32-00-410-010-A | Closing of the Thrust Reverser Halves |
| TASK 78-36-00-010-040-A | Opening of the Thrust Reverser Doors |
| TASK 78-36-00-010-040-B | Opening of the Thrust Reverser Doors |
| TASK 78-36-00-010-802-A | Opening of the Thrust Reverser Cowl-Doors |
| TASK 78-36-00-410-040-A | Closing of the Thrust Reverser Doors |
| TASK 78-36-00-410-040-B | Closing of the Thrust Reverser Doors |
| TASK 78-36-00-410-802-A | Closing of the Thrust Reverser Cowl-Doors |
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 28-21-00-941-053-A A. Safety Precautions
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 28-21-00-010-051-A ** ON A/C NOT FOR ALL 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.
B. Get Access
(1) Put an ACCESS PLATFORM 2M (6 FT) below the applicable access panels.
(2) Open the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-010-010).
(3) Open the thrust reverser cowl-doors:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Remove the applicable access panels:
(a) For the left wing, remove:
Subtask 28-21-00-010-051-B ** ON A/C NOT FOR ALL (1) Put an ACCESS PLATFORM 2M (6 FT) below the applicable access panels.
(2) Open the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-010-010).
(3) Open the thrust reverser cowl-doors:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Remove the applicable access panels:
(a) For the left wing, remove:
- 413AL, 413EL, 414FR and 413CL (Ref. AMM TASK 54-52-11-000-002).
- 414AZ, 471AL and 472AR (Ref. AMM TASK 54-53-11-000-002).
- 423AL, 423CL, 423FL and 424ER (Ref. AMM TASK 54-52-11-000-002).
- 423AZ, 481AL and 482AR (Ref. AMM TASK 54-53-11-000-002).
B. Get Access
(1) Put an ACCESS PLATFORM 2M (6 FT) below the applicable access panels.
(2) Open the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-010-040).
(3) Open the thrust reverser cowl-doors:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Remove the applicable access panels:
(a) For the left wing, remove:
Subtask 28-21-00-010-051-D ** ON A/C NOT FOR ALL (1) Put an ACCESS PLATFORM 2M (6 FT) below the applicable access panels.
(2) Open the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-010-040).
(3) Open the thrust reverser cowl-doors:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Remove the applicable access panels:
(a) For the left wing, remove:
- 413AL and 413CL (Ref. AMM TASK 54-52-11-000-002).
- 414AZ, 471AL, 471AR, 471BL and 471BR (Ref. AMM TASK 54-53-11-000-002).
- 423AL, 423CL and 423CR (Ref. AMM TASK 54-52-11-000-002).
- 423AZ, 481AL, 481AR, 481BL and 481BR (Ref. AMM TASK 54-53-11-000-002).
B. Get Access
(1) Put an ACCESS PLATFORM 2M (6 FT) in position below the applicable access panels.
(2) Open the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-010-802).
(3) Open the applicable thrust reverser cowl-doors:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Remove the applicable access panels:
(a) For the left wing, remove:
(b) For the right wing, remove:
Subtask 28-21-00-860-079-A (1) Put an ACCESS PLATFORM 2M (6 FT) in position below the applicable access panels.
(2) Open the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-010-802).
(3) Open the applicable thrust reverser cowl-doors:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Remove the applicable access panels:
(a) For the left wing, remove:
(b) For the right wing, remove:
C. Aircraft Maintenance Configuration
(2) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(3) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001), then:
(5) On the panel 115VU, put the ENG/MASTER 1 and the ENG/MASTER 2 switches in the ON position.
(6) On the ECAM lower DU:
Subtask 28-21-00-865-058-A WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
(1) On the panel 115VU, make sure that the ENG/MASTER 1 and the ENG/MASTER 2 switches are in the OFF position. (2) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(3) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001), then:
- on the ECAM control panel (CP), push (in) the FUEL pushbutton switch (P/BSW)
- make sure that the engine LP valves are shown closed (amber cross-line) on the ECAM lower display unit (DU).
(5) On the panel 115VU, put the ENG/MASTER 1 and the ENG/MASTER 2 switches in the ON position.
(6) On the ECAM lower DU:
- make sure that the engine LP valves are open (green in-line).
D. Open, safety and tag this(these) circuit breaker(s):
Subtask 28-21-00-860-080-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | FUEL/LP VALVE/MOT1/ENG2 | 2QG | A09 |
| 49VU | FUEL/LP VALVE/MOT1/ENG1 | 1QG | A08 |
| 121VU | FUEL/LP VALVE/MOT2/ENG2 | 4QG | M26 |
| 121VU | FUEL/LP VALVE/MOT2/ENG1 | 3QG | M25 |
E. Aircraft Maintenance Configuration (continued)
Panel Location ** ON A/C NOT FOR ALL
Panel Location ** ON A/C NOT FOR ALL
Panel Location ** ON A/C NOT FOR ALL
Fuel Pump System ** ON A/C NOT FOR ALL
Fuel Pump System ** ON A/C NOT FOR ALL
Fuel Pump System ** ON A/C NOT FOR ALL
(1) On the panel 115VU:
4. Procedure
Panel Location ** ON A/C NOT FOR ALL
Panel Location ** ON A/C NOT FOR ALL
Panel Location ** ON A/C NOT FOR ALL
Fuel Pump System ** ON A/C NOT FOR ALL
Fuel Pump System ** ON A/C NOT FOR ALL
Fuel Pump System ** ON A/C NOT FOR ALL - put the ENG/MASTER 1 and ENG/MASTER 2 switches in the OFF position.
- push (in) the L TK PUMPS 1 and 2 and the R TK PUMPS 1 and 2 P/BSW
- make sure that the OFF lights go off.
NOTE: The FAULT lights come on momentarily.
Subtask 28-21-00-790-053-A ** ON A/C NOT FOR ALL
A. Leak Test
(1) Examine the main fuel-feed pipeline from the LP valve to the fluid disconnect panel for fuel leaks:
(a) Make sure that there are no leaks.
Subtask 28-21-00-790-053-B ** ON A/C NOT FOR ALL (1) Examine the main fuel-feed pipeline from the LP valve to the fluid disconnect panel for fuel leaks:
(a) Make sure that there are no leaks.
A. Leak Test
(1) Examine the main fuel-feed line from the fuel double wall to the fluid disconnect panel for fuel leaks:
(a) Make sure that there are no leaks.
5. Close-up(1) Examine the main fuel-feed line from the fuel double wall to the fluid disconnect panel for fuel leaks:
(a) Make sure that there are no leaks.
Subtask 28-21-00-860-078-A
A. Aircraft Maintenance Configuration
(1) On the panel 40VU:
Subtask 28-21-00-865-057-A (1) On the panel 40VU:
- release (out) the L TK PUMPS 1 and 2 and R TK PUMPS 1 and 2 P/BSW
- make sure the OFF lights come on.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 28-21-00-860-083-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | FUEL/LP VALVE/MOT1/ENG2 | 2QG | A09 |
| 49VU | FUEL/LP VALVE/MOT1/ENG1 | 1QG | A08 |
| 121VU | FUEL/LP VALVE/MOT2/ENG2 | 4QG | M26 |
| 121VU | FUEL/LP VALVE/MOT2/ENG1 | 3QG | M25 |
C. 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 28-21-00-410-051-A ** ON A/C NOT FOR ALL (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).
D. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the removed access panels:
(a) For the left wing:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Close the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-410-010).
Subtask 28-21-00-410-051-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the removed access panels:
(a) For the left wing:
- 413AL, 413EL, 414FR and 413CL (Ref. AMM TASK 54-52-11-400-002).
- 414AZ, 471AL and 472AR (Ref. AMM TASK 54-53-11-400-002).
- 423AL, 423CL, 423FL and 424ER (Ref. AMM TASK 54-52-11-400-002).
- 423AZ, 481AL and 482AR (Ref. AMM TASK 54-53-11-400-002).
(a) For the left nacelle:
(b) For the right nacelle:
(4) Close the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-410-010).
D. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the removed access panels:
(a) For the left wing:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Close the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-410-040).
Subtask 28-21-00-410-051-D ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the removed access panels:
(a) For the left wing:
- 413AL and 413CL (Ref. AMM TASK 54-52-11-400-002).
- 414AZ, 471AL, 471AR, 471BL and 471BR (Ref. AMM TASK 54-53-11-400-002).
- 423AL, 423CL and 423CR (Ref. AMM TASK 54-52-11-400-002).
- 423AZ, 481AL, 481AR, 481BL and 481BR (Ref. AMM TASK 54-53-11-400-002).
(a) For the left nacelle:
(b) For the right nacelle:
(4) Close the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-410-040).
D. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access panels:
(a) For the left wing:
(b) For the right wing:
(3) Close the applicable thrust reverser cowl-doors:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Close the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-410-802).
Subtask 28-21-00-942-058-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access panels:
(a) For the left wing:
(b) For the right wing:
(3) Close the applicable thrust reverser cowl-doors:
(a) For the left nacelle:
(b) For the right nacelle:
(4) Close the fan cowl doors:
(a) 437AL and 447AL (Ref. AMM TASK 71-13-00-410-802).
E. 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.