Removal of the Refuel/Defuel Coupling-Element Assembly
TASK 28-25-41-000-005-A
Removal of the Refuel/Defuel Coupling-Element Assembly
Self explanatory
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 28-25-41-941-060-A
[Rev.10 from 2021]
2026.04.02 07:03:16 UTC
Removal of the Refuel/Defuel Coupling-Element Assembly
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.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 4M (13 FT) |
| No specific | 1 | CONTAINER 10 L(2 1/2 USGAL) |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 622KB | |
| 192MB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 28-00-00-910-001-A | Fuel Safety Procedures |
| TASK 57-41-37-000-006-A | Removal of the Access Panels |
Subtask 28-25-41-941-060-A
A. Safety Precautions
(2) Put the SAFETY BARRIER(S) in position.
Subtask 28-25-41-865-052-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 on the fuel system (Ref. AMM TASK 28-00-00-910-001). (2) Put the SAFETY BARRIER(S) in position.
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 28-25-41-010-060-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FUEL/RFL/DFL/SPLY | 2QU | L24 |
| 121VU | FUEL/RFL/DFL/XFR/DEFUEL/VALVE | 1QU | L23 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FUEL/RFL/DFL/SPLY | 2QU | L23 |
| 121VU | FUEL/RFL/DFL/XFR/DEFUEL/VALVE | 1QU | L22 |
C. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT) below the applicable refuel/defuel coupling 100QM(40QM).
(2) Remove the applicable access panel 522HB(622HB) (Ref. AMM TASK 57-41-37-000-006).
Subtask 28-25-41-010-060-B ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 4M (13 FT) below the applicable refuel/defuel coupling 100QM(40QM).
(2) Remove the applicable access panel 522HB(622HB) (Ref. AMM TASK 57-41-37-000-006).
C. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT) below the refuel/defuel coupling 40QM.
(2) Remove the access panel 622HB (Ref. AMM TASK 57-41-37-000-006).
Subtask 28-25-41-860-056-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 4M (13 FT) below the refuel/defuel coupling 40QM.
(2) Remove the access panel 622HB (Ref. AMM TASK 57-41-37-000-006).
D. Aircraft Maintenance Configuration
(1) Open access door 192MB.
(2) On refuel/defuel control-panel 800VU:
(a) Put the MODE SELECT switch in the OFF position and lower the guard:
1 Make sure that the DEFUEL/XFR valve is in shut position (light 21QU goes off).
(b) Put all the REFUEL VALVES switches in the NORM position and lower the guard.
(3) Close access door 192MB.
Subtask 28-25-41-860-056-B ** ON A/C NOT FOR ALL (1) Open access door 192MB.
(2) On refuel/defuel control-panel 800VU:
(a) Put the MODE SELECT switch in the OFF position and lower the guard:
1 Make sure that the DEFUEL/XFR valve is in shut position (light 21QU goes off).
(b) Put all the REFUEL VALVES switches in the NORM position and lower the guard.
(3) Close access door 192MB.
NOTE: If the door is operated in battery power, Airbus recommends you not to open the door more than the necessary time. If you keep the door open for a longer time the battery power decreases.
D. Aircraft Maintenance Configuration
(1) Open access door 622KB.
(2) On refuel/defuel control-panel 800VU:
(a) Put the MODE SELECT switch in the OFF position and lower the guard:
1 Make sure that the DEFUEL/XFR valve is in shut position (light 21QU goes off).
(b) Put all the REFUEL VALVES switches in the NORM position and lower the guard.
(3) Close access door 622KB.
4. Procedure(1) Open access door 622KB.
(2) On refuel/defuel control-panel 800VU:
(a) Put the MODE SELECT switch in the OFF position and lower the guard:
1 Make sure that the DEFUEL/XFR valve is in shut position (light 21QU goes off).
(b) Put all the REFUEL VALVES switches in the NORM position and lower the guard.
(3) Close access door 622KB.
NOTE: If the door is operated in battery power, Airbus recommends you not to open the door more than the necessary time. If you keep the door open for a longer time the battery power decreases.
WARNING:
BE CAREFUL NOT TO GET AIRCRAFT FUEL IN YOUR MOUTH OR IN YOUR EYES.
IF YOU GET FUEL ON YOUR SKIN OR ON YOUR CLOTHES, FLUSH IT IMMEDIATELY WITH WATER.
IF NECESSARY, GET MEDICAL HELP.
AIRCRAFT FUEL IS POISONOUS.
Subtask 28-25-41-020-063-A A. Removal of the Refuel/Defuel Coupling-Element Assembly
(1) Do the steps that follow, if:
(c) Remove the lanyard (9) from the attachment lug on the shroud ring (5).
(d) Remove the coupling cap (8) with the lanyard (9).
(e) Put a CONTAINER 10 L(2 1/2 USGAL) below the coupling (1).
(f) Manually operate the check valve (in the element assembly (4)) to drain the remaining fuel into the CONTAINER 10 L(2 1/2 USGAL).
(g) Remove the CONTAINER 10 L(2 1/2 USGAL).
(h) Discard the drained fuel in the approved area.
(i) Hold the element assembly (4) and remove the bolts (7) and the washers (6).
(j) Remove the shroud ring (5), the element assembly (4) and the laminated shim(s) (3).
(k) Remove and discard the O-ring (2).
(2) Do the steps that follow, if:
(c) Remove the lanyard (9) from the attachment lug on the shroud ring (5).
(d) Remove the coupling cap (8) with the lanyard (9).
(e) Hold the element assembly (4) and remove the bolts (7) and the washers (6).
(f) Put a CONTAINER 10 L(2 1/2 USGAL) below the coupling (1).
(g) Carefully remove the shroud ring (5) and the element assembly (4):
1 Momentarily drain the remaining fuel into the CONTAINER 10 L(2 1/2 USGAL).
(h) Remove the CONTAINER 10 L(2 1/2 USGAL).
(i) Discard the drained fuel in the approved area.
(j) Remove the laminated shim(s) (3).
(k) Remove and discard the O-ring (2).
Subtask 28-25-41-020-064-A (1) Do the steps that follow, if:
- The check valve in the element assembly is operational
- The coupling cap is connected to the coupling with a lanyard.
NOTE: The coupling cap (8) will hang by the lanyard (9) from the shroud ring (5).
(b) Remove the nut (11) and the screw (10).(c) Remove the lanyard (9) from the attachment lug on the shroud ring (5).
(d) Remove the coupling cap (8) with the lanyard (9).
(e) Put a CONTAINER 10 L(2 1/2 USGAL) below the coupling (1).
(f) Manually operate the check valve (in the element assembly (4)) to drain the remaining fuel into the CONTAINER 10 L(2 1/2 USGAL).
(g) Remove the CONTAINER 10 L(2 1/2 USGAL).
(h) Discard the drained fuel in the approved area.
(i) Hold the element assembly (4) and remove the bolts (7) and the washers (6).
(j) Remove the shroud ring (5), the element assembly (4) and the laminated shim(s) (3).
(k) Remove and discard the O-ring (2).
(2) Do the steps that follow, if:
- The check valve in the element assembly is not operational
- The coupling cap is connected to the coupling with a lanyard.
NOTE: The coupling cap (8) will hang by the lanyard (9) from the shroud ring (5).
(b) Remove the nut (11) and the screw (10).(c) Remove the lanyard (9) from the attachment lug on the shroud ring (5).
(d) Remove the coupling cap (8) with the lanyard (9).
(e) Hold the element assembly (4) and remove the bolts (7) and the washers (6).
(f) Put a CONTAINER 10 L(2 1/2 USGAL) below the coupling (1).
(g) Carefully remove the shroud ring (5) and the element assembly (4):
1 Momentarily drain the remaining fuel into the CONTAINER 10 L(2 1/2 USGAL).
(h) Remove the CONTAINER 10 L(2 1/2 USGAL).
(i) Discard the drained fuel in the approved area.
(j) Remove the laminated shim(s) (3).
(k) Remove and discard the O-ring (2).
B. Removal of the Refuel/Defuel Coupling-Element Assembly
(1) Do the steps that follow, if:
(d) Put a CONTAINER 10 L(2 1/2 USGAL) below the coupling (21).
(e) Manually operate the check valve (in the element assembly (24)) to drain the remaining fuel into the CONTAINER 10 L(2 1/2 USGAL).
(f) Remove the CONTAINER 10 L(2 1/2 USGAL).
(g) Discard the drained fuel in the approved area.
(h) Hold the element assembly (24) and remove the remaining bolts (27) and the washers (26).
(i) Remove the shroud ring (25), the element assembly (24) and the laminated shim(s) (23).
(j) Remove and discard the O-ring (22).
(2) Do the steps that follow, if:
(d) Hold the element assembly (24) and remove the remaining bolts (27) and the washers (26).
(e) Put a CONTAINER 10 L(2 1/2 USGAL) below the coupling (21).
(f) Carefully remove the shroud ring (25) and the element assembly (24:
1 Momentarily drain the remaining fuel into the CONTAINER 10 L(2 1/2 USGAL).
(g) Remove the CONTAINER 10 L(2 1/2 USGAL).
(h) Discard the drained fuel in the approved area.
(i) Remove the laminated shim(s) (23).
(j) Remove and discard the O-ring (22).
(1) Do the steps that follow, if:
- The check valve in the element assembly is operational
- The coupling cap is connected to the coupling with a chain.
NOTE: The coupling cap (28) will hang by the chain (29) from the shroud ring (25).
(b) Remove the bolt (27) that attaches the attachment tag (30) to the shroud ring (25). NOTE: The attachment tag (30) will stay connected to the chain (29).
(c) Remove the coupling cap (28) with the chain (29). (d) Put a CONTAINER 10 L(2 1/2 USGAL) below the coupling (21).
(e) Manually operate the check valve (in the element assembly (24)) to drain the remaining fuel into the CONTAINER 10 L(2 1/2 USGAL).
(f) Remove the CONTAINER 10 L(2 1/2 USGAL).
(g) Discard the drained fuel in the approved area.
(h) Hold the element assembly (24) and remove the remaining bolts (27) and the washers (26).
(i) Remove the shroud ring (25), the element assembly (24) and the laminated shim(s) (23).
(j) Remove and discard the O-ring (22).
(2) Do the steps that follow, if:
- The check valve in the element assembly is not operational
- The coupling cap is connected to the coupling with a chain.
NOTE: The coupling cap (28) will hang by the chain (29) from the shroud ring (25).
(b) Remove the bolt (27) that attaches the attachment tag (30) to the shroud ring (25). NOTE: The attachment tag (30) will stay connected to the chain (29).
(c) Remove the coupling cap (28) with the chain (29). (d) Hold the element assembly (24) and remove the remaining bolts (27) and the washers (26).
(e) Put a CONTAINER 10 L(2 1/2 USGAL) below the coupling (21).
(f) Carefully remove the shroud ring (25) and the element assembly (24:
1 Momentarily drain the remaining fuel into the CONTAINER 10 L(2 1/2 USGAL).
(g) Remove the CONTAINER 10 L(2 1/2 USGAL).
(h) Discard the drained fuel in the approved area.
(i) Remove the laminated shim(s) (23).
(j) Remove and discard the O-ring (22).
Refuel/Defuel Coupling Element Assembly - Location and Detail