W DOC AIRBUS | AMM A320F

Removal of the Return Fuel Lines [PW11]


TASK 73-11-48-000-803-A
Removal of the Return Fuel Lines


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
WARNING: WEAR APPLICABLE PERSONAL PROTECTIVE EQUIPMENT (PPE) WHEN YOU DO THIS TASK. BEFORE YOU USE PPE, READ, UNDERSTAND AND OBEY ALL INSTRUCTIONS FOR ITS USE. THESE INSTRUCTIONS INCLUDE INSTRUCTIONS FROM THE MANUFACTURER, YOUR EMPLOYER AND GOVERNMENT REGULATIONS. YOU CAN GET INJURED IF YOU DO NOT USE PPE. GET INSTRUCTIONS FROM YOUR EMPLOYER ON WHICH PPE IS NECESSARY.
WARNING: DO NOT LET THE ENGINE FUEL SPILL ON THE ENGINE. YOU MUST IMMEDIATELY REMOVE UNWANTED FUEL. THE FUEL IS FLAMMABLE AND CAN CAUSE INJURY OR DAMAGE.
WARNING: DO NOT LET ENGINE FUEL STAY ON YOUR SKIN FOR A LONG TIME. FLUSH THE FUEL FROM YOUR SKIN WITH WATER. THE FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY.
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
1
CONTAINER 20L (5 USGAL)
No specific
AR
COVER - PROTECTION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WRENCH - STANDARD
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR, 451AL
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR, 461AL
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 31-60-00-860-001-A
EIS Start Procedure
TASK 71-00-00-860-833-A
Procedure to Prevent Engine Motoring
TASK 71-13-00-010-802-A
Opening of the Fan Cowl Doors
TASK 78-30-00-040-805-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-36-00-010-802-A
Opening of the Thrust Reverser Cowl-Doors
3. Job Set-up
Subtask 73-11-48-941-071-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Do the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833)
Subtask 73-11-48-860-058-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
   (2) Make sure that on the SD ENG fuel page, the LP valve is shown closed.
Subtask 73-11-48-865-059-A ** ON A/C NOT FOR ALL
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENG 1)
49VUFUEL/LP VALVE/MOT1/ENG11QGA08
121VUFUEL/LP VALVE/MOT2/ENG13QGM25
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
49VUFUEL/LP VALVE/MOT1/ENG22QGA09
121VUFUEL/LP VALVE/MOT2/ENG24QGM26
Subtask 73-11-48-010-062-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR
Subtask 73-11-48-040-052-A ** ON A/C NOT FOR ALL
E. Deactivation of the Thrust Reverser for Ground Maintenance
WARNING: YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE AN INJURY AND/OR DAMAGE.
   (1) Do the deactivation of the thrust reverser system for ground maintenance (Ref. AMM TASK 78-30-00-040-805).
Subtask 73-11-48-010-063-A ** ON A/C NOT FOR ALL
F. Get Access
   (1) Open the left thrust reverser cowl-door (Ref. AMM TASK 78-36-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL
   (2) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position.
4. Procedure
Subtask 73-11-48-020-054-A ** ON A/C NOT FOR ALL
CAUTION: WIPE CLEAN ALL PARTS AND TOOLS AS NECESSARY TO REMOVE UNWANTED DEBRIS AND PREVENT DAMAGE TO THE ENGINE.
CAUTION: USE A SECOND WRENCH TO HOLD THE MATING PARTS WHEN YOU LOOSEN OR TIGHTEN THE TUBE OR HOSE NUTS. IF YOU DO NOT OBEY THIS INSTRUCTION, YOU CAN TWIST THE TUBES OR HOSES OR CAUSE DAMAGE TO THEM.
A. Removal of the Return Fuel Lines
NOTE: Use a second WRENCH - STANDARD when you loosen or tighten the tube or hose nuts.
   (1) Remove the elbow (5).
     (a) Remove the bolt (2), washer (3) and clamp (4) that attach the lower fuel return tube (1) to the lower fuel bracket.
     (b) Put a CONTAINER 20L (5 USGAL) below the elbow (5) on the fuel return valve.
     (c) Disconnect the elbow (5) from the fuel return valve.
     (d) Drain the remaining fuel from the lower fuel return tube (1) and the fuel return valve into the container.
     (e) Remove the elbow (5) from the lower fuel return tube (1).
   (2) Remove the lower fuel return tube (1).
     (a) Remove the bolt (8), washer (7) and clamp (6) that attach the lower fuel return tube (1) to the middle fuel bracket.
     (b) Disconnect the lower fuel return tube (1) from the upper fuel return tube (12).
     (c) Remove the lower fuel return tube (1).
   (3) Remove the upper fuel return tube (12).
     (a) Remove the bolt (10), washer (11) and clamp (9) that attach the upper fuel return tube (12) to the harness bracket.
     (b) Remove the bolt (14), washer (11) and clamp (13) that attach the upper fuel return tube (12) to the return fuel bracket.
     (c) Remove the bolt (17), washer (16) and clamp (18) that attach the upper fuel return tube (12) to the return fuel bracket.
     (d) Disconnect the upper fuel return tube (12) from the return fuel hose (15).
     (e) Remove the upper fuel return tube (12).
   (4) Remove the return fuel hose (15).
     (a) Disconnect the return fuel hose (15) from the pylon interface.
     (b) Remove the return fuel hose (15).
   (5) Installation of the protection covers
CAUTION: INSTALL PROTECTION COVERS ON ALL THE OPENINGS IMMEDIATELY TO PREVENT DAMAGE TO THE ENGINE.
     (a) Install COVER - PROTECTION on the elbow (5), the lower fuel return tube (1), the upper fuel return tube (12) and the return fuel hose (15).
     (b) Install COVER - PROTECTION on the pylon interface and on the return valve.
[Rev.10 from 2021] 2026.04.01 13:14:41 UTC