W DOC AIRBUS | AMM A320F

Installation of the Primary and Secondary Fuel-Manifold (131-9(A))


TASK 49-31-42-400-006-A
Installation of the Primary and Secondary Fuel-Manifold (131-9(A))


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
SAFETY CLIP - CIRCUIT BREAKER
No specific
Torque wrench: range to between 38.5 and 31.5 lbf.in (0.44 and 0.36 m.daN ) T
No specific
Torque wrench: range to between 1.49 and 1.23 m.daN (131.86 and 108.85 lbf.in ) T
No specific
Torque wrench: range to between 1.738 and 1.422 m.daN (12.82 and 10.49 lbf.ft ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
315AL, 316AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 52-41-00-010-001-A
Open the APU Doors for Access
3. Job Set-up
Subtask 49-31-42-860-058-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
   (2) On the panel 25VU, make sure that the APU MASTER SW p/bsw is OFF.
   (3) Make sure that there is a warning notice in the cockpit to tell persons not to start the APU.
   (4) Make sure that the hydraulic systems are depressurized
(Ref. AMM TASK 29-00-00-864-001).
   (5) Make sure that the access platform is in position below the APU compartment.
   (6) Make sure that the APU access doors are open (Ref. AMM TASK 52-41-00-010-001).
   (7) Make sure that the LIGHT control SW 11LJ is set to the ON position.
Subtask 49-31-42-865-062-A ** ON A/C NOT FOR ALL
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUAPU/APU/CTL2KDL42
121VUAPU/ECB/SPLY1KDL41
4. Procedure
Subtask 49-31-42-420-056-A ** ON A/C NOT FOR ALL
A. Install the Primary and Secondary fuel manifold assembly.
   (1) Install the primary (1) and secondary (2) manifold on the APU.
   (2) Connect the manifolds at the fuel nozzles (4) and the fuel flow divider (3).
   (3) TORQUE the fittings at the fuel nozzles (4) to between 1.49 and 1.23 m.daN (131.86 and 108.85 lbf.in ) T.
   (4) TORQUE the fittings at the fuel flow divider (3) to between 1.738 and 1.422 m.daN (12.82 and 10.49 lbf.ft )
T.
Subtask 49-31-42-420-056-B ** ON A/C NOT FOR ALL 5. Close-up
Subtask 49-31-42-410-053-A ** ON A/C NOT FOR ALL
Subtask 49-31-42-865-063-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUAPU/APU/CTL2KDL42
121VUAPU/ECB/SPLY1KDL41
Subtask 49-31-42-860-059-A ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
   (1) Put the related hydraulic system in the pressurized configuration (Ref. AMM TASK 29-00-00-864-001).
   (2) De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 01:29:41 UTC