W DOC AIRBUS | AMM A320F

Air Leak Test with closed APU Doors


TASK 49-00-00-790-006-A
Air Leak Test with closed APU Doors


WARNING: DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS WHEN YOU DO THE MAINTENANCE TASK(S).
ZONE: 315
ZONE: 316
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
 B. Consumable Materials
REFERENCE
DESIGNATION
CP3010
dry developer
(Material No.08CKB9)
Cleaner-Hydraulic Spillage Absorbent powder -
(Material No.14QFB1)
Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
315
TAIL CONE APU AND ACCESSORY COMPARTMENT
316
TAIL CONE APU AND ACCESSORY COMPARTMENT
315AL, 316AR
 D. 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 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 49-00-00-860-008-A
APU Start by External Power
TASK 49-00-00-860-008-A-01
APU Start by Batteries
TASK 49-00-00-860-009-A
APU Shutdown by External Power (131-9(A))
TASK 49-00-00-860-009-A-01
APU Shutdown by Batteries (131-9(A))
TASK 52-41-00-010-001-A
Open the APU Doors for Access
TASK 52-41-00-410-001-A
Close the APU Doors after Access
3. Job Set-up
Subtask 49-00-00-860-105-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) On the panel 25VU, make sure that the APU MASTER SW p/bsw is OFF.
   (3) Put 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).
Subtask 49-00-00-865-115-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
Subtask 49-00-00-010-071-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put the access platform in position below the APU access doors 315AL and 316AR.
   (2) Open the APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
   (3) Set the LIGHT control SW 11LJ to the ON position.
4. Procedure
Subtask 49-00-00-480-056-A ** ON A/C NOT FOR ALL
A. Preparation for the Leak Test
   (1) There are two possible procedures to find the location of a pneumatic joint air leak. You can apply CP3010 dry developer or Cleaner-Hydraulic Spillage Absorbent powder - (Material No.08CKB9) and dry around the pneumatic joints. Or you can install aluminum foil around the pneumatic joint location. Use the steps that follow to apply aluminum foil to the pneumatic joint locations:
     (a) Wind the foil wrap around the joint one time.
     (b) Twist the seam of the foil wrap tight as shown.
     (c) Make the foil wrap as tight as possible on the tube but do not rip the wrap.
     (d) Attach the foil wrap with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - at both sides of the pneumatic joint.
Subtask 49-00-00-410-075-A ** ON A/C NOT FOR ALL
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Set the LIGHT control SW 11LJ to the OFF position.
   (3) Close the APU access doors 316AR 315AL and (Ref. AMM TASK 52-41-00-410-001).
   (4) Remove the access platform(s).
   (5) Remove the WARNING NOTICE(S).
Subtask 49-00-00-865-116-A ** ON A/C NOT FOR ALL
C. 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 49-00-00-790-055-A ** ON A/C NOT FOR ALL
D. Air Leak Test
   (1) Start the APU (Ref. AMM TASK 49-00-00-860-008).
   (2) During APU operation:
  • supply bleed air.
   (3) Stop the APU (Ref. AMM TASK 49-00-00-860-009).
   (4) Put a warning notice in the cockpit to tell persons not to start the APU.
Subtask 49-00-00-865-117-A ** ON A/C NOT FOR ALL
E. 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 49-00-00-010-072-A ** ON A/C NOT FOR ALL
F. Get Access
   (1) Put the access platform in position below the APU access doors 315AL and 316AR.
   (2) Open the APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
   (3) Set the LIGHT control SW 11LJ to the ON position.
Subtask 49-00-00-080-056-A ** ON A/C NOT FOR ALL
G. Make sure that there no leaks at the joint location, and remove the materials used to check leaks.
5. Close-up
Subtask 49-00-00-410-076-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) Set the LIGHT control SW 11LJ to the OFF position.
   (3) Close the APU access doors 316AR 315AL (Ref. AMM TASK 52-41-00-410-001).
   (4) Remove the access platform(s).
Subtask 49-00-00-865-118-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 49-00-00-860-106-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 aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 12:43:10 UTC