W DOC AIRBUS | AMM A320F

Installation of the Fuel Distribution Valve Filter [IAE]


TASK 73-13-43-400-011-B
Installation of the Fuel Distribution Valve Filter


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
ACCESS PLATFORM 1M(3 FT)
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 75 and 70 lbf.in (0.85 and 0.79 m.daN ) T
No specific
Torque wrench: range to between 95 and 85 lbf.in (1.07 and 0.96 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.V02-141)
corrosion resistant steel lockwire
(Material No.V10-066)
liquid paraffin
(Material No.V10-067)
lubricant
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
RING
AIPC 73-11-49-74-020
1
PACKING
AIPC 73-13-43-81-140
9
PACKING
AIPC 73-13-43-81-160
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 70-23-11-911-013-A
General Torque Tightening Techniques
TASK 70-23-13-911-010-A
Procedures for the Installation of Preformed Packings
TASK 70-40-11-911-014-A
Locking Devices General Information
TASK 71-00-00-710-012-B
Test No.3 : Idle Leak Check
TASK 71-00-00-710-046-B
Test No.2 : Wet Motor Leak Check
TASK 71-13-00-010-010-A
Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-010-A
Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 78-30-00-040-012-A
Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance
TASK 78-30-00-440-012-A
Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after Ground Maintenance
TASK 78-32-00-010-010-A
Opening of the Thrust Reverser Halves
TASK 78-32-00-410-010-A
Closing of the Thrust Reverser Halves
3. Job Set-up
Subtask 73-13-43-860-053-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) On the center pedestal, on the ENG panel 115VU, make sure that a WARNING NOTICE(S) is in position to tell persons not to start the engine.
   (2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that a WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).
   (3) Make sure that the ACCESS PLATFORM 1M(3 FT) is in position.
Subtask 73-13-43-010-061-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that the fan cowls are open: (Ref. AMM TASK 71-13-00-010-010)
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Make sure that the thrust reverser doors are open: (Ref. AMM TASK 78-32-00-010-010)
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 73-13-43-040-057-A ** ON A/C NOT FOR ALL
C. Make sure that the thrust reverser Hydraulic Control Unit (HCU) is deactivated (Ref. AMM TASK 78-30-00-040-012)
4. Procedure
Subtask 73-13-43-420-062-A ** ON A/C NOT FOR ALL
A. Installation of the fuel distribution valve filter
   (1) Install the filter:
     (a) Lubricate a new AIPC 73-13-43-81-160 PACKING (9) with liquid paraffin (Material No.V10-066) and install it on the filter (8) (Ref. AMM TASK 70-23-13-911-010).
     (b) Install the filter in the fuel distribution valve housing.
   (2) Install the filter cover:
     (a) Install a new packing.
CAUTION: FILTER COVER PACKING (1) IS MADE FROM A SPECIAL MATERIAL THAT PREVENTS OVER-HEATING. DO NOT USE AN ALTERNATIVE SEAL.
       1 Lubricate a new AIPC 73-13-43-81-140 PACKING (1) with liquid paraffin (Material No.V10-066) and install it on the filter cover (7) (Ref. AMM TASK 70-23-13-911-010).
     (b) Align the eight offset bolt holes.
     (c) Lubricate the threads of the eight bolts (5) with lubricant (Material No.V10-067) .
     (d) Install the bolts (5) and the eight washers (6) that attach the filter cover to the fuel distribution valve (10).
     (e) TORQUE the bolts (5) to between 75 and 70 lbf.in (0.85 and 0.79 m.daN ) T (Ref. AMM TASK 70-23-11-911-013).
   (3) Install the fuel inlet line
     (a) Lubricate a new AIPC 73-11-49-74-020 RING (2) with liquid paraffin (Material No.V10-066) and install it on the fuel inlet line (3) (Ref. AMM TASK 70-23-13-911-010).
     (b) Install the fuel inlet line between the lower bifurcation panel and filter cover.
     (c) Attach and torque the connection at the bifurcation panel.
     (d) Install the three bolts (4) that attach the fuel inlet line to the filter cover.
     (e) TORQUE the bolts (4) to between 95 and 85 lbf.in (1.07 and 0.96 m.daN ) T (Ref. AMM TASK 70-23-11-911-013).
     (f) Safety the bolts with corrosion resistant steel lockwire (Material No.V02-141) (Ref. AMM TASK 70-40-11-911-014).
5. Close-up
Subtask 73-13-43-410-056-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 thrust reverser halves (Ref. AMM TASK 78-32-00-410-010):
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR.
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
Subtask 73-13-43-440-053-A ** ON A/C NOT FOR ALL
B. Activate the thrust reverser HCU (Ref. AMM TASK 78-30-00-440-012).
Subtask 73-13-43-410-057-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010)
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
Subtask 73-13-43-790-055-A ** ON A/C NOT FOR ALL
D. Test Requirements
   (1) Do an idle leak check (Ref. AMM TASK 71-00-00-710-012).
NOTE: A wet motor leak check (Ref. AMM TASK 71-00-00-710-046) may be used to check for leaks, but this must be followed by an idle leak check (Ref. AMM TASK 71-00-00-710-012).
[Rev.10 from 2021] 2026.04.01 03:00:37 UTC