W DOC AIRBUS | AMM A320F

Removal of the Fuel Return Valve (FRV) [CFMB]


TASK 73-11-50-000-002-A
Removal of the Fuel Return Valve (FRV)


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
CAP - BLANKING
No specific
AR
CONTAINER 5 L (1.32 USGAL)
No specific
AR
PLIERS - CONNECTOR, JAW, SOFT
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
3. Job Set-up
Subtask 73-11-50-941-056-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) On the center pedestal, on the ENG panel 115VU:
     (a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
   (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
   (3) On the overhead maintenance panel 50VU:
     (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 73-11-50-861-051-A ** ON A/C NOT FOR ALL
B. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 73-11-50-865-053-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: 1000EM1 (ENGINE1)
49VUFUEL/LP VALVE/MOT1/ENG11QGA08
121VUFUEL/LP VALVE/MOT2/ENG13QGM25
FOR FIN: 1000EM2 (ENGINE2)
49VUFUEL/LP VALVE/MOT1/ENG22QGA09
121VUFUEL/LP VALVE/MOT2/ENG24QGM26
Subtask 73-11-50-010-057-A ** ON A/C NOT FOR ALL
D. Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
   (1) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (2) FOR [1000EM2] (ENGINE-2)
447AL 448AR
4. Procedure
Subtask 73-11-50-020-053-A ** ON A/C NOT FOR ALL
A. Removal of the Fuel Return Valve
CAUTION: INSTALL CAPS AND PLUGS ON THE ORIFICES OF ALL DISCONNECTED PIPES AND PARTS FOR THEIR PROTECTION AGAINST CONTAMINATION BY UNWANTED MATERIALS.
CAUTION: USE TWO WRENCHES TO REMOVE OR INSTALL THE TUBE COUPLING NUTS:
  • ONE WRENCH TO HOLD THE UNION, AND
  • ONE TO LOOSEN OR TIGHTEN THE COUPLING NUT.
THIS PREVENTS DAMAGE TO THE PARTS.
   (1) Install a CONTAINER 5 L (1.32 USGAL) under the fuel return valve and loosen the fuel return tube (10) coupling nut to drain the fuel which remains in the tube.

PRE SB CFM 73-0096

   (2) Disconnect the fuel tubes which follow:
     (a) Fuel return tube (10).
     (b) Shutoff signal (PB/PSF) fuel tube (30).
     (c) Fuel pump HP tube (40).
     (d) IDG cooler tube (50).
     (e) Fuel pump LP tube (60).
     (f) Drain tube (90)

END OF PRE SB CFM 73-0096



POST SB CFM 73-0096

   (3) Disconnect the fuel tubes which follow:
     (a) Fuel return tube (10).
     (b) Bypass (PB/PSF) fuel tube (30).
     (c) Fuel pump HP tube (40).
     (d) IDG cooler tube (50).
     (e) Fuel pump LP tube (60).
     (f) Drain tube (90)

END OF SB CFM 73-0096

   (4) Disconnect the HJ7 harness connector (70) and the HJ8 harness connector (80). Use PLIERS - CONNECTOR, JAW, SOFT only if necessary.
   (5) Remove the FRV
CAUTION: TAKE CARE DURING REMOVAL OF THE FUEL RETURN VALVE NOT TO DAMAGE THE NIPPLES.
     (a) Remove the 4 bolts (100) and washers (110) which attach the FRV on bracket (20), between flanges E and F at the 10 o'clock position.
     (b) Remove the FRV from the engine.
     (c) Install CAP - BLANKING on the disconnected parts and orifices.
[Rev.10 from 2021] 2026.04.01 02:58:07 UTC