DOC AIRBUS | AMM A320FInstallation of the Fuel Pump Canister
TASK 28-21-52-400-002-A
Installation of the Fuel Pump Canister
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 28-21-52-941-062-A
Subtask 28-21-52-560-051-A ** ON A/C NOT FOR ALL
Subtask 28-21-52-410-051-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:17:28 UTC
Installation of the Fuel Pump Canister
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
WARNING:
THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL). CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
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
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | Torque wrench: range to between 0.9 and 0.8 m.daN (79.65 and 70.80 lbf.in )  |
| 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 |
|---|---|
| 540 | FUEL TANK |
| 640 | FUEL TANK |
| 540AB, 540BZ, 640AB, 640BZ | |
| FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR) | |
| 540AB, 540BZ | |
| FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR) | |
| 640AB, 640BZ | |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 11 | SEALING RING | AIPC 28-21-05-27-040 |
| 12 | SEALING RING | AIPC 28-21-05-27-040 |
| 11 | O-RING | AIPC 28-21-05-27-120 |
| 17 | O-RING | AIPC 28-21-05-27-120 |
| 19 | O-RING | AIPC 28-21-05-28-160 |
| 39 | O-RING | AIPC 28-21-05-28-160 |
| 17 | O-RING | AIPC 28-21-05-29-050 |
| 19 | O-RING | AIPC 28-21-05-29-050 |
| 33 | O-RING | AIPC 28-21-05-35-120 |
| 11 | SEALING RING | AIPC 28-21-85-22-040 |
| 17 | O-RING | AIPC 28-21-85-22-230 |
| 39 | O-RING | AIPC 28-21-85-23-200 |
| 19 | O-RING | AIPC 28-21-85-24-050 |
| 33 | O-RING | AIPC 28-21-85-26-070 |
| 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 28-00-00-400-001-A | Installation 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 28-21-43-400-002-A | Installation of the Fuel-Pump Check-Valve |
| TASK 28-21-45-400-003-A | Installation of the Sequence Valve |
| TASK 28-21-51-000-001-A | Removal of the Fuel Pumps |
| TASK 28-21-51-400-001-A | Installation 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 57-27-11-000-001-A | Removal of the Access Panel |
| TASK 57-27-11-400-001-A | Installation of the Access Panel |
| TASK 57-27-12-000-002-A | Removal of the Rib 2 Access Panel 540AZ(640AZ) or 540BZ(640BZ) |
| FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR) | |
| TASK 57-27-11-400-001-A | Installation of the Access Panel |
| TASK 57-27-12-400-002-A | Installation of the Rib 2 Access Panel 540AZ (640AZ) or 540BZ (640BZ) |
| FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR) | |
| TASK 57-27-11-400-001-A | Installation of the Access Panel |
| TASK 57-27-12-400-002-A | Installation of the Rib 2 Access Panel 540AZ (640AZ) or 540BZ (640BZ) |
Fuel-Pump Canister 1QM (4QM) and 2QM (3QM)Subtask 28-21-52-941-062-A
A. Safety Procedures
(2) Make sure that the SAFETY BARRIER(S) are in position.
Subtask 28-21-52-865-051-A 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) 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 28-21-52-860-051-A ** ON A/C NOT FOR ALL | 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 |
C. Aircraft Maintenance Configuration
(1) Make sure that the applicable fuel tank is defueled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is below the applicable zone 540(640).
(4) Make sure that the applicable access panel 540AB(640AB) is removed (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 28-10-00-910-002).
(5) Make sure that the applicable RIB 2 surge door 540BZ(640BZ) is open and that the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) is installed on the door.
Subtask 28-21-52-860-051-B ** ON A/C NOT FOR ALL (1) Make sure that the applicable fuel tank is defueled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is below the applicable zone 540(640).
(4) Make sure that the applicable access panel 540AB(640AB) is removed (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 28-10-00-910-002).
(5) Make sure that the applicable RIB 2 surge door 540BZ(640BZ) is open and that the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) is installed on the door.
C. Aircraft Maintenance Configuration
(1) Make sure that the applicable fuel tank is defueled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is below the applicable zone 540 (640).
(4) Make sure that the applicable access panel 540AB ( 640AB) is removed (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 28-10-00-910-002).
(5) Make sure that the applicable RIB2 access panel 540BZ ( 640BZ) is removed (Ref. AMM TASK 57-27-12-000-002).
(6) Make sure that the applicable fuel pump 22QA (25QA) is removed (Ref. AMM TASK 28-21-51-000-001).
4. Procedure(1) Make sure that the applicable fuel tank is defueled (Ref. AMM TASK 28-25-00-650-001).
(2) Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is below the applicable zone 540 (640).
(4) Make sure that the applicable access panel 540AB ( 640AB) is removed (Ref. AMM TASK 57-27-11-000-001) and (Ref. AMM TASK 28-10-00-910-002).
(5) Make sure that the applicable RIB2 access panel 540BZ ( 640BZ) is removed (Ref. AMM TASK 57-27-12-000-002).
(6) Make sure that the applicable fuel pump 22QA (25QA) is removed (Ref. AMM TASK 28-21-51-000-001).
Subtask 28-21-52-560-051-A ** ON A/C NOT FOR ALL
A. Preparation for a Replacement Component
(1) Remove the plug (25).
(2) Remove and discard the O-ring (26).
(3) Lubricate the new AIPC 28-21-05-27-120 O-RING (11) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(4) Install the new O-ring (11).
(5) Install the reducer (10).
(6) Install the sequence valve (Ref. AMM TASK 28-21-45-400-003).
Subtask 28-21-52-420-057-A ** ON A/C NOT FOR ALL (1) Remove the plug (25).
(2) Remove and discard the O-ring (26).
(3) Lubricate the new AIPC 28-21-05-27-120 O-RING (11) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(4) Install the new O-ring (11).
(5) Install the reducer (10).
(6) Install the sequence valve (Ref. AMM TASK 28-21-45-400-003).
B. 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 items that follow with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) :
Subtask 28-21-52-560-051-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 items that follow with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) :
C. Preparation for a Replacement Component
(1) Remove the plug (42).
(2) Remove and discard the O-ring (43).
(3) Lubricate the new AIPC 28-21-05-27-120 O-RING (17) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(4) Install the new O-ring (17).
(5) Install the reducer (18).
(6) Install the fuel pump check-valve (Ref. AMM TASK 28-21-43-400-002).
Subtask 28-21-52-420-057-B ** ON A/C NOT FOR ALL (1) Remove the plug (42).
(2) Remove and discard the O-ring (43).
(3) Lubricate the new AIPC 28-21-05-27-120 O-RING (17) with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(4) Install the new O-ring (17).
(5) Install the reducer (18).
(6) Install the fuel pump check-valve (Ref. AMM TASK 28-21-43-400-002).
D. 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 items that follow with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) :
Subtask 28-21-52-560-051-D ** 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 items that follow with Turbine Fuel-- Kerosene - (Material No.01ABA1) or Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) :
E. Preparation for a Replacement Component
(1) Remove the plug (43).
(2) Remove and discard the O-ring (44).
(3) Lubricate the new AIPC 28-21-05-27-120 O-RING (17) or AIPC 28-21-85-22-230 O-RING (17) with Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(4) Install the new O-ring (17).
(5) Install the reducer (18).
(6) Install the fuel pump check-valve (Ref. AMM TASK 28-21-43-400-002).
Subtask 28-21-52-420-057-D ** ON A/C NOT FOR ALL (1) Remove the plug (43).
(2) Remove and discard the O-ring (44).
(3) Lubricate the new AIPC 28-21-05-27-120 O-RING (17) or AIPC 28-21-85-22-230 O-RING (17) with Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) .
(4) Install the new O-ring (17).
(5) Install the reducer (18).
(6) Install the fuel pump check-valve (Ref. AMM TASK 28-21-43-400-002).
F. 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 items that follow with Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) :
Subtask 28-21-52-420-052-D ** 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 items that follow with Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) :
- The AIPC 28-21-05-27-040 SEALING RING (11) or AIPC 28-21-85-22-040 SEALING RING (11)
- The AIPC 28-21-05-29-050 O-RING (19) or AIPC 28-21-85-24-050 O-RING (19)
- The AIPC 28-21-05-35-120 O-RING (33) or AIPC 28-21-85-26-070 O-RING (33)
- The AIPC 28-21-05-28-160 O-RING (39) or AIPC 28-21-85-23-200 O-RING (39).
G. Installation of the Fuel Pump Canister 2QM(3QM)
(1) Install the new sealing ring (12) and the new O-rings (17) and (19).
(2) Engage the connectors (16) and (14), while you put the canister (15) in position.
(3) Install the canister (15) with the screws (13).
.
(5) Make sure that one of the screws (13) is correctly bonded:
(6) Install the connector (16) with the bolts (21) and the nuts (20).
(8) Install the connector (14) with the bolts (21) and the nuts (20).
(9) Install the pipe (9).
Subtask 28-21-52-420-052-E ** ON A/C NOT FOR ALL (1) Install the new sealing ring (12) and the new O-rings (17) and (19).
(2) Engage the connectors (16) and (14), while you put the canister (15) in position.
(3) Install the canister (15) with the screws (13).
NOTE: You must bond one of the screws (13) (Ref. AMM TASK 20-28-00-912-802).
(4) TORQUE the screws (13) to between 0.9 and 0.8 m.daN (79.65 and 70.80 lbf.in ) . (5) Make sure that one of the screws (13) is correctly bonded:
WARNING:
THIS INSTRUCTION IS APPLICABLE TO A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) ITEM. CAREFULLY OBEY ALL GIVEN INSTRUCTIONS WHEN YOU DO THIS STEP. IF YOU DO NOT OBEY THESE INSTRUCTIONS, A DANGEROUS CONDITION CAN OCCUR THAT CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
(a) Do a bonding check of one of the screws (13) (Ref. AMM TASK 20-28-00-912-802). The bonding resistance must be less than 10 milliohms. (6) Install the connector (16) with the bolts (21) and the nuts (20).
NOTE: You must bond one of the bolts (21) (Ref. AMM TASK 20-28-00-912-802).
(7) Make sure that one of the bolts (21) is correctly bonded: WARNING:
THIS INSTRUCTION IS APPLICABLE TO A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) ITEM. CAREFULLY OBEY ALL GIVEN INSTRUCTIONS WHEN YOU DO THIS STEP. IF YOU DO NOT OBEY THESE INSTRUCTIONS, A DANGEROUS CONDITION CAN OCCUR THAT CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
(a) Do a bonding check between one of the bolts (21) and the canister (15) (Ref. AMM TASK 20-28-00-912-802). The bonding resistance must be less than 10 milliohms. (8) Install the connector (14) with the bolts (21) and the nuts (20).
(9) Install the pipe (9).
G. Installation of the Fuel Pump Canister 2QM(3QM)
(1) Install the new sealing ring (11) and the new O-rings (19), (33) and (39).
(2) Install the canister (15) with the screws (12).
.
(4) Make sure that one of the screws (12) is correctly bonded:
(5) Install the connector (13). Install the bolts (40) and the nuts (38).
(6) Install the bolt (41), the bonding tab (36) and the nut (37) (Ref. AMM TASK 20-28-00-912-802).
(7) Make sure that the bonding tab (36) is correctly bonded:
(8) Install the connector (14). Install the bolts (34) and the nuts (31).
(9) Install the bolt (35), the bonding tab (29) and the nut (30) (Ref. AMM TASK 20-28-00-912-802).
(10) Make sure that the bonding tab (29) is correctly bonded:
(11) Install the connector (16). Install the bolts (22) and the nuts (21).
(13) Install the fuel pipes that you removed (Ref. AMM TASK 28-00-00-400-001).
(14) Install the pipe (9).
(15) Apply Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) to the bolts (22), (34) and (40) and to the nuts (21), (31) and (38).
5. Close-up(1) Install the new sealing ring (11) and the new O-rings (19), (33) and (39).
(2) Install the canister (15) with the screws (12).
NOTE: You must bond one of the screws (12) (Ref. AMM TASK 20-28-00-912-802).
(3) TORQUE the screws (12) to between 0.9 and 0.8 m.daN (79.65 and 70.80 lbf.in ) . (4) Make sure that one of the screws (12) is correctly bonded:
WARNING:
THIS INSTRUCTION IS APPLICABLE TO A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) ITEM. CAREFULLY OBEY ALL GIVEN INSTRUCTIONS WHEN YOU DO THIS STEP. IF YOU DO NOT OBEY THESE INSTRUCTIONS, A DANGEROUS CONDITION CAN OCCUR THAT CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
(a) Do a bonding check of one of the screws (12) (Ref. AMM TASK 20-28-00-912-802). The bonding resistance must be less than 10 milliohms. (5) Install the connector (13). Install the bolts (40) and the nuts (38).
(6) Install the bolt (41), the bonding tab (36) and the nut (37) (Ref. AMM TASK 20-28-00-912-802).
(7) Make sure that the bonding tab (36) is correctly bonded:
WARNING:
THIS INSTRUCTION IS APPLICABLE TO A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) ITEM. CAREFULLY OBEY ALL GIVEN INSTRUCTIONS WHEN YOU DO THIS STEP. IF YOU DO NOT OBEY THESE INSTRUCTIONS, A DANGEROUS CONDITION CAN OCCUR THAT CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
(a) Do a bonding check between the bonding tab (36) and the canister (15) (Ref. AMM TASK 20-28-00-912-802). The bonding resistance must be less than 10 milliohms. (8) Install the connector (14). Install the bolts (34) and the nuts (31).
(9) Install the bolt (35), the bonding tab (29) and the nut (30) (Ref. AMM TASK 20-28-00-912-802).
(10) Make sure that the bonding tab (29) is correctly bonded:
WARNING:
THIS INSTRUCTION IS APPLICABLE TO A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) ITEM. CAREFULLY OBEY ALL GIVEN INSTRUCTIONS WHEN YOU DO THIS STEP. IF YOU DO NOT OBEY THESE INSTRUCTIONS, A DANGEROUS CONDITION CAN OCCUR THAT CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
(a) Do a bonding check between the bonding tab (29) and the canister (15) (Ref. AMM TASK 20-28-00-912-802). The bonding resistance must be less than 10 milliohms. (11) Install the connector (16). Install the bolts (22) and the nuts (21).
NOTE: You must bond one of the bolts (22)> (Ref. AMM TASK 20-28-00-912-802).
(12) Make sure that one of the bolts (22) is correctly bonded: WARNING:
THIS INSTRUCTION IS APPLICABLE TO A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) ITEM. CAREFULLY OBEY ALL GIVEN INSTRUCTIONS WHEN YOU DO THIS STEP. IF YOU DO NOT OBEY THESE INSTRUCTIONS, A DANGEROUS CONDITION CAN OCCUR THAT CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
(a) Do a bonding check between one of the bolts (22) and the canister (15) (Ref. AMM TASK 20-28-00-912-802). The bonding resistance must be less than 10 milliohms. (13) Install the fuel pipes that you removed (Ref. AMM TASK 28-00-00-400-001).
(14) Install the pipe (9).
(15) Apply Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) to the bolts (22), (34) and (40) and to the nuts (21), (31) and (38).
Subtask 28-21-52-410-051-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 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) and make sure that the applicable RIB 2 surge door is closed:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
540BZ
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
640BZ.
(3) Install the applicable wing-access panel (Ref. AMM TASK 57-27-11-400-001):
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
install 540AB
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
install 640AB.
(4) Install the applicable fuel pump 22QA(25QA) (Ref. AMM TASK 28-21-51-400-001).
Subtask 28-21-52-410-051-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the 98D57004014000 HOOK-COVER (RIB2-SURGE DOORS) and make sure that the applicable RIB 2 surge door is closed:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
540BZ
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
640BZ.
(3) Install the applicable wing-access panel (Ref. AMM TASK 57-27-11-400-001):
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
install 540AB
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
install 640AB.
(4) Install the applicable fuel pump 22QA(25QA) (Ref. AMM TASK 28-21-51-400-001).
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable fuel pump 22QA (25QA) (Ref. AMM TASK 28-21-51-400-001).
(3) Install the applicable RIB2 access panels that follow:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
Install 540BZ (Ref. AMM TASK 57-27-12-400-002).
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
Install 640BZ (Ref. AMM TASK 57-27-12-400-002).
(4) Install the applicable wing access panels that follow:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
Install 540AB (Ref. AMM TASK 57-27-11-400-001).
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
Install 640AB (Ref. AMM TASK 57-27-11-400-001).
Subtask 28-21-52-865-057-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable fuel pump 22QA (25QA) (Ref. AMM TASK 28-21-51-400-001).
(3) Install the applicable RIB2 access panels that follow:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
Install 540BZ (Ref. AMM TASK 57-27-12-400-002).
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
Install 640BZ (Ref. AMM TASK 57-27-12-400-002).
(4) Install the applicable wing access panels that follow:
(a) FOR [2QM] (CANISTER-FUEL PUMP, L WING TK INR)
Install 540AB (Ref. AMM TASK 57-27-11-400-001).
(b) FOR [3QM] (CANISTER-FUEL PUMP, R WING TK INR)
Install 640AB (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 28-21-52-650-057-A | 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 |
C. Fuel Configuration
(1) 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 28-21-52-942-053-A (1) 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).
D. 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.