DOC AIRBUS | AMM A320FInstallation of the Fuel Pump Strainer
TASK 28-21-54-400-001-A
Installation of the Fuel Pump Strainer
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 28-21-54-941-053-A ** ON A/C NOT FOR ALL
Subtask 28-21-54-420-050-B ** ON A/C NOT FOR ALL
Subtask 28-21-54-410-050-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:17:30 UTC
Installation of the Fuel Pump Strainer
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.
FIN: 5QM ** ON A/C NOT FOR ALL
FIN: 6QM ** ON A/C NOT FOR ALL
FIN: 7QM ** ON A/C NOT FOR ALL
FIN: 8QM ** ON A/C NOT FOR ALL
1. Reason for the JobFIN: 6QM ** ON A/C NOT FOR ALL
FIN: 7QM ** ON A/C NOT FOR ALL
FIN: 8QM ** ON A/C NOT FOR ALL
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) |
| No specific | 1 | ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.01ABA1) | Turbine Fuel-- Kerosene - |
| (Material No.03FAB1) | Mineral Oil base Grease-- Vaseline or Petrolatum - |
| (Material No.06ABA1) | Polysulfide Sealant-Fuel Tank Brushable - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ | |
| FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR) | |
| FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR) | |
| 540AZ, 640AZ | |
| FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR) | |
| FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR) | |
| 540AB | |
| FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR) | |
| FOR [8QM] (STRAINER-PUMP INLET, R WING TK OUTR) | |
| 540BZ, 640BZ | |
| FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR) | |
| FOR [8QM] (STRAINER-PUMP INLET, R WING TK OUTR) | |
| 640AB | |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 2 | O-RING | AIPC 28-21-05-28-160 |
| 2 | O-RING | AIPC 28-21-85-23-200 |
| 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 28-10-00-910-001-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 28-25-00-650-001-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 57-27-11-000-001-A | Removal of the Access Panel |
| TASK 57-27-11-400-001-A | Installation of the Access Panel |
| FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR) | |
| FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR) | |
| TASK 57-27-12-000-002-A | Removal of the Rib 2 Access Panel 540AZ(640AZ) or 540BZ(640BZ) |
| TASK 57-27-12-400-002-A | Installation of the Rib 2 Access Panel 540AZ (640AZ) or 540BZ (640BZ) |
| FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR) | |
| FOR [6QM] (STRAINER-PUMP INLET, 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 57-27-11-400-001-A | Installation of the Access Panel |
| FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR) | |
| FOR [8QM] (STRAINER-PUMP INLET, R WING TK OUTR) | |
| TASK 57-27-12-000-002-A | Removal of the Rib 2 Access Panel 540AZ(640AZ) or 540BZ(640BZ) |
| TASK 57-27-12-400-002-A | Installation of the Rib 2 Access Panel 540AZ (640AZ) or 540BZ (640BZ) |
| FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR) | |
| FOR [8QM] (STRAINER-PUMP INLET, R WING TK OUTR) | |
| 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 57-27-11-400-001-A | Installation of the Access Panel |
Fuel Pump StrainerSubtask 28-21-54-941-053-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(2) Make sure that the SAFETY BARRIER(S) are in position.
Subtask 28-21-54-865-052-A ** ON A/C NOT FOR ALL 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 (Ref. AMM TASK 28-10-00-910-001) when you do work in a fuel tank. (2) Make sure that the SAFETY BARRIER(S) are in position.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 28-21-54-860-052-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR 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 |
C. Aircraft Maintenance Configuration
(1) Make sure that the center tank and the applicable wing fuel tank are defuelled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable wing fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable access panel 540AB(640AB).
(4) Make sure that the applicable access panel 540AB(640AB) is removed (Ref. AMM TASK 28-10-00-910-002), (Ref. AMM TASK 57-27-11-000-001).
(5) Make sure that the applicable surge door is open:
(a) FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
the surge door 540BZ(640BZ)
(b) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [7QM] (STRAINER-PUMP INLET, R WING TK INR)
the surge door 540AZ(640AZ).
(6) Make sure that the applicable tool is on the surge door:
Subtask 28-21-54-860-052-B ** ON A/C NOT FOR ALL (1) Make sure that the center tank and the applicable wing fuel tank are defuelled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable wing fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable access panel 540AB(640AB).
(4) Make sure that the applicable access panel 540AB(640AB) is removed (Ref. AMM TASK 28-10-00-910-002), (Ref. AMM TASK 57-27-11-000-001).
(5) Make sure that the applicable surge door is open:
(a) FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
the surge door 540BZ(640BZ)
(b) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [7QM] (STRAINER-PUMP INLET, R WING TK INR)
the surge door 540AZ(640AZ).
(6) Make sure that the applicable tool is on the surge door:
- For 540BZ(640BZ) the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS)
- For 540AZ(640AZ) the 98D57004013000 HOOK-COVER (RIB 2 SURGE DOORS).
C. Aircraft Maintenance Configuration
(1) Make sure that the center tank and the applicable wing fuel tank are defueled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable wing fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position below the applicable access panels that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [6QM] (STRAINER-PUMP INLET, L WING TK INR)
Below 540AB.
(b) FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Below 640AB.
(4) Make sure that the applicable access panels are removed that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [6QM] (STRAINER-PUMP INLET, L WING TK INR)
Remove 540AB (Ref. AMM TASK 28-10-00-910-002) and (Ref. AMM TASK 57-27-11-000-001).
(b) FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Remove 640AB (Ref. AMM TASK 28-10-00-910-002) and (Ref. AMM TASK 57-27-11-000-001).
(5) Make sure that the applicable RIB2 access panels are removed that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [7QM] (STRAINER-PUMP INLET, R WING TK INR)
Remove 540AZ ( 640AZ) (Ref. AMM TASK 57-27-12-000-002).
(b) FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Remove 540BZ ( 640BZ) (Ref. AMM TASK 57-27-12-000-002).
4. Procedure(1) Make sure that the center tank and the applicable wing fuel tank are defueled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable wing fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position below the applicable access panels that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [6QM] (STRAINER-PUMP INLET, L WING TK INR)
Below 540AB.
(b) FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Below 640AB.
(4) Make sure that the applicable access panels are removed that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [6QM] (STRAINER-PUMP INLET, L WING TK INR)
Remove 540AB (Ref. AMM TASK 28-10-00-910-002) and (Ref. AMM TASK 57-27-11-000-001).
(b) FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Remove 640AB (Ref. AMM TASK 28-10-00-910-002) and (Ref. AMM TASK 57-27-11-000-001).
(5) Make sure that the applicable RIB2 access panels are removed that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [7QM] (STRAINER-PUMP INLET, R WING TK INR)
Remove 540AZ ( 640AZ) (Ref. AMM TASK 57-27-12-000-002).
(b) FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Remove 540BZ ( 640BZ) (Ref. AMM TASK 57-27-12-000-002).
Subtask 28-21-54-420-050-B ** ON A/C NOT FOR ALL
A. Preparation for Installation
(1) Clean the component interfaces and the adjacent areas 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 28-21-05-28-160 O-RING (2) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
Subtask 28-21-54-420-050-C ** ON A/C NOT FOR ALL (1) Clean the component interfaces and the adjacent areas 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 28-21-05-28-160 O-RING (2) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
A. Preparation for Installation
(1) Clean the component interfaces and the adjacent areas 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 28-21-05-28-160 O-RING (2) or AIPC 28-21-85-23-200 O-RING (2) with Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
Subtask 28-21-54-420-051-B ** ON A/C NOT FOR ALL (1) Clean the component interfaces and the adjacent areas 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 28-21-05-28-160 O-RING (2) or AIPC 28-21-85-23-200 O-RING (2) with Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
B. Installation of the Fuel Pump Strainer
(1) Put the strainer (15) in position on the bracket (10) and install the bolts (9).
(2) Install a new O-ring (2) on the fuel pipe (1).
(3) Install the nut (4) and the retaining ring (3) on the fuel pipe (1).
(4) Install the filter connector (5) on the strainer (15) with the bolts (6).
(5) Install the fuel pipe (1) in the filter connector (5). Tighten the nut (4) onto the filter connector (5) to keep the fuel pipe (1) in position.
(6) Position the cowls (12) and (7) on the bracket (10) and install the three bolts (13).
(7) Install the two bolts (8).
(8) Position the bonding tab (11) on the cowl (12) and install the bolt (14) (Ref. AMM TASK 20-28-00-912-802).
(9) Apply Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) to the bolts (6), (8), (9) and (13).
5. Close-up(1) Put the strainer (15) in position on the bracket (10) and install the bolts (9).
(2) Install a new O-ring (2) on the fuel pipe (1).
(3) Install the nut (4) and the retaining ring (3) on the fuel pipe (1).
(4) Install the filter connector (5) on the strainer (15) with the bolts (6).
(5) Install the fuel pipe (1) in the filter connector (5). Tighten the nut (4) onto the filter connector (5) to keep the fuel pipe (1) in position.
(6) Position the cowls (12) and (7) on the bracket (10) and install the three bolts (13).
(7) Install the two bolts (8).
(8) Position the bonding tab (11) on the cowl (12) and install the bolt (14) (Ref. AMM TASK 20-28-00-912-802).
(9) Apply Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) to the bolts (6), (8), (9) and (13).
Subtask 28-21-54-410-050-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the applicable tool 98D57004013000 HOOK-COVER (RIB 2 SURGE DOORS) or 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).
(3) Close the applicable fuel-surge access door 540AZ 640AZ 540BZ 640BZ.
(4) Install the applicable access panel 540AB 640AB (Ref. AMM TASK 28-10-00-910-002) (Ref. AMM TASK 57-27-11-400-001).
Subtask 28-21-54-410-050-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the applicable tool 98D57004013000 HOOK-COVER (RIB 2 SURGE DOORS) or 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS).
(3) Close the applicable fuel-surge access door 540AZ 640AZ 540BZ 640BZ.
(4) Install the applicable access panel 540AB 640AB (Ref. AMM TASK 28-10-00-910-002) (Ref. AMM TASK 57-27-11-400-001).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable RIB2 access panels that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [7QM] (STRAINER-PUMP INLET, R WING TK INR)
Install 540AZ ( 640AZ) (Ref. AMM TASK 57-27-12-400-002).
(b) FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Install 540BZ ( 640BZ) (Ref. AMM TASK 57-27-12-400-002).
(3) Install the applicable access panels that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [6QM] (STRAINER-PUMP INLET, L WING TK INR)
Install 540AB (Ref. AMM TASK 28-10-00-910-002) and (Ref. AMM TASK 57-27-11-400-001).
(b) FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Install 640AB (Ref. AMM TASK 28-10-00-910-002) and (Ref. AMM TASK 57-27-11-400-001).
Subtask 28-21-54-865-051-A ** 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 applicable RIB2 access panels that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [7QM] (STRAINER-PUMP INLET, R WING TK INR)
Install 540AZ ( 640AZ) (Ref. AMM TASK 57-27-12-400-002).
(b) FOR [6QM] (STRAINER-PUMP INLET, L WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Install 540BZ ( 640BZ) (Ref. AMM TASK 57-27-12-400-002).
(3) Install the applicable access panels that follow:
(a) FOR [5QM] (STRAINER-PUMP INLET, L WING TK OUTR), [6QM] (STRAINER-PUMP INLET, L WING TK INR)
Install 540AB (Ref. AMM TASK 28-10-00-910-002) and (Ref. AMM TASK 57-27-11-400-001).
(b) FOR [7QM] (STRAINER-PUMP INLET, R WING TK INR), [8QM] (STRAINER-PUMP INLET, R WING TK OUTR)
Install 640AB (Ref. AMM TASK 28-10-00-910-002) and (Ref. AMM TASK 57-27-11-400-001).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 28-21-54-650-051-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR 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 |
C. Fuel Configuration
(1) Refuel, defuel or transfer fuel as applicable (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 28-21-54-942-050-A ** ON A/C NOT FOR ALL (1) Refuel, defuel or transfer fuel as applicable (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).
D. Removal of Equipment
(1) Remove the safety barriers.
(2) Remove the WARNING NOTICE(S).
(3) Remove the access platform(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 WARNING NOTICE(S).
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.