Removal of the Fuel Pump Canister

TASK 28-21-52-000-002-A
Removal of the Fuel Pump Canister

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.

ZONE: 540
ZONE: 640
FIN: 2QM
FIN: 3QM

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	ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific	AR	SAFETY BARRIER(S)
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	Torque wrench: range to between 4.64 and 3.87 m.daN (34.22 and 28.54 lbf.ft )
98D57004014000	1	HOOK-COVER (RIB2-SURGE DOORS)

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.01ABA1)	Turbine Fuel-- Kerosene -
(Material No.03FAB1)	Mineral Oil base Grease-- Vaseline or Petrolatum -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
540	FUEL TANK
640	FUEL TANK
FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
540AB, 540BZ
FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
640AB, 640BZ

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
26	O-RING	AIPC 28-21-05-27-120
43	O-RING	AIPC 28-21-05-27-120

E. 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 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 28-00-00-000-001-A	Removal of the Fuel Pipes
TASK 28-10-00-910-001-A	Safety Procedures When You Do Work in a Fuel Tank
TASK 28-10-00-910-002-A	Access to the Fuel Tanks and the Work Areas
TASK 28-21-43-000-002-A	Removal of the Fuel-Pump Check-Valve
TASK 28-21-45-000-001-A	Removal of the Sequence Valve
TASK 28-21-51-000-001-A	Removal of the Fuel Pumps
TASK 28-25-00-650-001-A	Pressure Defuel
TASK 28-25-00-650-003-A	To Drain Remaining Fuel from the Wing Tanks and the Center Tank
TASK 28-25-00-650-003-A-01	To Drain Remaining Fuel from the Wing Tanks and the Center Tank
TASK 28-25-00-869-001-A	Fuel Transfer
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 57-27-11-000-001-A	Removal of the Access Panel
Fuel-Pump Canister 1QM (4QM) and 2QM (3QM) ** ON A/C NOT FOR ALL
Fuel-Pump Canister 1QM (4QM) and 2QM (3QM) ** ON A/C NOT FOR ALL
Fuel Pump Canister 1QM (4QM) and 2QM (3QM) ** ON A/C NOT FOR ALL
Fuel Pump Canister 1QM (4QM) and 2QM (3QM) ** ON A/C NOT FOR ALL
FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
TASK 28-10-00-910-002-A	Access to the Fuel Tanks and the Work Areas
TASK 57-27-11-000-001-A	Removal of the Access Panel
TASK 57-27-12-000-002-A	Removal of the Rib 2 Access Panel 540AZ(640AZ) or 540BZ(640BZ)
FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
TASK 28-10-00-910-002-A	Access to the Fuel Tanks and the Work Areas
TASK 57-27-11-000-001-A	Removal of the Access Panel
TASK 57-27-12-000-002-A	Removal of the Rib 2 Access Panel 540AZ(640AZ) or 540BZ(640BZ)

3. Job Set-up
Subtask 28-21-52-941-059-A

A. Safety Procedures

WARNING: BEFORE YOU DO WORK IN OR NEAR A FUEL TANK, MAKE SURE THAT YOU OBEY ALL THE SAFETY PROCEDURES. THIS WILL PREVENT INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.

(1) You must obey the fuel safety procedures when you do work in a fuel tank (Ref. AMM TASK 28-10-00-910-001).
(2) Put the SAFETY BARRIER(S) in position.

Subtask 28-21-52-650-054-A ** ON A/C NOT FOR ALL

B. Fuel Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Defuel the fuel from the applicable wing tank (Ref. AMM TASK 28-25-00-650-001) or transfer the fuel from the applicable wing tank (Ref. AMM TASK 28-25-00-869-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) In the cockpit, on the ECAM control panel, push (in) the FUEL system-page button.

CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.

(5) In the cockpit, on fuel panel 40VU, release (out) the X FEED pushbutton switch (the ON and OPEN lights go off).
(6) In the cockpit, on the ECAM lower Display Unit (DU), make sure that the X FEED valve indication shows the green cross-line (closed).
(7) In the cockpit, on the ECAM control panel, turn the LOWER DISPLAY switch counterclockwise to the off position:
(a) Make sure that the ECAM lower DU goes off.
(8) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(9) Drain the remaining fuel from the applicable wing tank (Ref. AMM TASK 28-25-00-650-003).

Subtask 28-21-52-650-054-B ** ON A/C NOT FOR ALL

B. Fuel Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Defuel the fuel from the applicable wing tank and the center tank (Ref. AMM TASK 28-25-00-650-001) or transfer the fuel from the applicable wing tank and the center tank (Ref. AMM TASK 28-25-00-869-001).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) In the cockpit, on the ECAM control panel, push (in) the FUEL system-page button.

CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.

Subtask 28-21-52-865-054-A

C. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	FUEL/CTR TK/PUMP2 SPLY	30QA	P26
121VU	FUEL/CTR TK/PUMP1 SPLY	29QA	P23
** ON A/C ALL
121VU	FUEL/L WING TK/PUMP2 SPLY	7QA	N26
121VU	FUEL/L WING TK/PUMP1 SPLY	1QA	N23
121VU	FUEL/R WING TK/PUMP2 SPLY	8QA	Q26
121VU	FUEL/R WING TK/PUMP1 SPLY	2QA	Q23
123VU	L WING TK/PUMP 1/STBY SPLY	11QA	AD12
123VU	R WING TK/PUMP 1/STBY SPLY	12QA	AE12

Subtask 28-21-52-010-054-A ** ON A/C NOT FOR ALL

D. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE below the applicable zone 540(640).
(2) Remove the applicable fuel pump 22QA(25QA) (Ref. AMM TASK 28-21-51-000-001).
(3) Remove the applicable wing access panel (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 28-10-00-910-002):
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
remove 540AB
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
remove 640AB.
(4) Open the applicable RIB 2 surge door:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
open 540BZ
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
open 640BZ.
(5) Install the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).

Subtask 28-21-52-010-054-B ** ON A/C NOT FOR ALL

D. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE below the applicable zone 540 (640).
(2) Remove the applicable wing access panels that follow:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
Remove 540AB (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 28-10-00-910-002).
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
Remove 640AB (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 28-10-00-910-002).
(3) Remove the applicable RIB2 access panels that follow:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
Remove 540BZ (Ref. AMM TASK 57-27-12-000-002).
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
Remove 640BZ (Ref. AMM TASK 57-27-12-000-002).
(4) Remove the applicable fuel pump 22QA (25QA) (Ref. AMM TASK 28-21-51-000-001).

4. Procedure
Subtask 28-21-52-020-056-A ** ON A/C NOT FOR ALL

A. Removal of Fuel Pump Canister 2QM (3QM)
(1) Disconnect the pipe (9).
(2) Remove the nuts (20) and the bolts (21).
(3) Remove the screws (13).
(4) Release the connectors (14) and (16).
(5) Remove and discard the O-rings (17) and (19).
(6) Remove the canister (15).
(7) Remove and discard the sealing ring (12).
(8) If you are to replace the canister (15), do as follows:
(a) Remove the sequence valve (Ref. AMM TASK 28-21-45-000-001).
(b) Remove the reducer (10).
(c) Remove and discard the O-ring (11).
(9) Lubricate the new AIPC 28-21-05-27-120 O-RING (26) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(10) Install the O-ring (26) and the plug (25).

Fuel Pump Canister 1QM (4QM) and 2QM (3QM) ** ON A/C NOT FOR ALL

(11) TORQUE the plug (25) to between 4.64 and 3.87 m.daN (34.22 and 28.54 lbf.ft )

Subtask 28-21-52-020-056-C ** ON A/C NOT FOR ALL

A. Removal of Fuel Pump Canister 2QM (3QM)
(1) Disconnect the pipe (9).
(2) Remove the nuts (38) and the bolts (40).
(3) Remove the nut (37), the bonding tab (36) (with its bonding strap) and the bolt (41).
(4) Remove the nuts (31) and the bolts (34).
(5) Remove the nut (30), the bonding tab (29) (with its bonding strap) and the bolt (35).
(6) Remove the nuts (21) and the bolts (22).
(7) Remove the fuel pipes as necessary (Ref. AMM TASK 28-00-00-000-001), so that you can remove the connectors (13), (14) and (16).
(8) Remove the connectors (13), (14) and (16).
(9) Remove and discard the O-rings (39), (33) and (19).
(10) Remove the screws (12).
(11) Remove the canister (15).
(12) Remove and discard the sealing ring (11).
(13) If you are to replace the canister (15), do as follows:
(a) Remove the check valve (Ref. AMM TASK 28-21-43-000-002).
(b) Remove the reducer (18).
(c) Remove and discard the O-ring (17).
(14) Lubricate the new AIPC 28-21-05-27-120 O-RING (43) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(15) Install the O-ring (43) and the plug (42).

Fuel Pump Canister 1QM (4QM) and 2QM (3QM) ** ON A/C NOT FOR ALL

(16) TORQUE the plug (42) to between 4.64 and 3.87 m.daN (34.22 and 28.54 lbf.ft )

[Rev.10 from 2021] 2026.04.02 06:17:27 UTC