W DOC AIRBUS | AMM A320F

Installation of the Fuel Recovery Tank [PW11]


TASK 73-13-01-400-801-A
Installation of the Fuel Recovery Tank


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AND THE ADJACENT COMPONENTS AFTER ENGINE SHUTDOWN. THE ENGINE, THE ENGINE OIL AND THE ADJACENT COMPONENTS CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 400
1. Reason for the Job
Use this procedure to install the fuel recovery tank.
For more information about the engine fuel and control system, refer to (73-00-00-00U).
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
COVER - PROTECTION
No specific
Torque wrench: range to between 75 and 65 lbf.in (0.85 and 0.73 m.daN ) T
No specific
Torque wrench: range to between 100 and 90 lbf.in (1.13 and 1.02 m.daN ) T
No specific
Torque wrench: range to between 225 and 200 lbf.in (2.54 and 2.26 m.daN ) T
No specific
Torque wrench: range to between 375 and 340 lbf.in (4.24 and 3.84 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.P06-054)
Antigalling Compound
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR, 452AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR, 462AR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 71-00-00-720-811-A
Test No. 3A - Idle Power Test
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 71-13-00-410-802-A
Closing of the Fan Cowl Doors
TASK 72-21-08-400-801-A
Installation of the Fan Exit Liner Segments
TASK 78-30-00-040-805-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-30-00-440-805-A
Reactivation of the Thrust Reverser System after Ground Maintenance
TASK 78-36-00-010-802-A
Opening of the Thrust Reverser Cowl-Doors
TASK 78-36-00-410-802-A
Closing of the Thrust Reverser Cowl-Doors
3. Job Set-up
Subtask 73-13-01-941-051-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Make sure that you did the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833).
Subtask 73-13-01-010-052-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that the fan cowl doors are open (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 73-13-01-040-051-A ** ON A/C NOT FOR ALL
C. Deactivation of the Thrust Reverser System for 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) Make sure that you did the deactivation of the thrust reverser system for maintenance (Ref. AMM TASK 78-30-00-040-805).
Subtask 73-13-01-010-053-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Make sure that the right thrust reverser cowl-doors are open (Ref. AMM TASK 78-36-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
452AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
462AR
4. Procedure
CAUTION: WIPE CLEAN ALL PARTS AND TOOLS AS NECESSARY TO REMOVE UNWANTED DEBRIS AND PREVENT DAMAGE TO THE ENGINE.
Subtask 73-13-01-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Fuel Recovery Tank
   (1) Removal of the protection covers
CAUTION: REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY TO PREVENT ENGINE DAMAGE.
     (a) Make sure that you remove all the necessary COVER - PROTECTION to prevent damage to the engine.
   (2) Install the fuel recovery tank (1) as follows:
     (a) Apply Antigalling Compound (Material No.P06-054) to the two bolts (2) and the two bolts (3).
NOTE: For new or refurbished bolts or nuts with baked-on lubricant, do not do the wet application.
     (b) Install the tank (1) to the bracket with the two bolts (2).
     (c) Install the tank (1) to the Low Pressure Compressor (LPC) with the two bolts (3).
     (d) TORQUE the two bolts (2) to between 100 and 90 lbf.in (1.13 and 1.02 m.daN ) T.
     (e) TORQUE the two bolts (3) to between 100 and 90 lbf.in (1.13 and 1.02 m.daN )
T.

POST SB C-73-00-0010A (Config-2: Fuel Drainage Improvement Configuration)

     (f) Install the metering plug (4) to the tank (1).

END OF POST SB C-73-00-0010A (Config-2: Fuel Drainage Improvement Configuration)

   (3) Connection of the fuel tubes
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 CAUTION, YOU CAN TWIST OR CAUSE DAMAGE TO THE TUBES OR HOSES.
     (a) Connect the fuel tubes (FB01), (FD02) and (FD03) to the tank (1).
     (b) Torque the fuel tube (FB01) as follows:
       1 TORQUE the B-nut to between 75 and 65 lbf.in (0.85 and 0.73 m.daN )
T.
     (c) Torque the fuel tube (FD02) as follows:
       1 TORQUE the B-nut to between 375 and 340 lbf.in (4.24 and 3.84 m.daN )
T.
     (d) Torque the fuel tube (FD03) as follows:
       1 TORQUE the B-nut to between 225 and 200 lbf.in (2.54 and 2.26 m.daN )
T.
   (4) Do an idle test (
Ref. AMM TASK 71-00-00-720-811).
   (5) Install the fan exit liner and duct segment at the 6 o'clock position (Ref. AMM TASK 72-21-08-400-801).
   (6) Examine the assembly for foreign objects, damage and correct assembly.
   (7) Installation of the protection covers.
CAUTION: INSTALL PROTECTION COVERS ON ALL THE OPENINGS IMMEDIATELY TO PREVENT DAMAGE TO THE ENGINE.
     (a) Make sure that you install COVER - PROTECTION as necessary to prevent damage to the engine.
5. Close-up
Subtask 73-13-01-410-050-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) Close the right thrust reverser cowl-doors (Ref. AMM TASK 78-36-00-410-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
452AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
462AR
Subtask 73-13-01-440-050-A ** ON A/C NOT FOR ALL
B. Do the reactivation of the thrust reverser system after maintenance (Ref. AMM TASK 78-30-00-440-805).
Subtask 73-13-01-410-051-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 03:02:20 UTC