W DOC AIRBUS | AMM A320F

Installation of the APU Substitution Kit (APS 3200)


TASK 49-11-00-400-003-A
Installation of the APU Substitution Kit (APS 3200)


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION: MAKE SURE THAT AN APU SUBSTITUTION KIT IS INSTALLED WHEN THE AIRCRAFT IS TO FLY WITHOUT AN APU INSTALLED. THIS IS A TEMPORARY PROCEDURE TO:
  • ATTACH THE MOUNTING STRAPS AND ELECTRICAL CABLES
  • INSTALL BLANKING CAPS
UNTIL THE SERVICEABLE APU IS INSTALLED.
1. Reason for the Job
Installation of the APU Substitution Kit
Do this task only after you did the deactivation procedure of the APU by the APU substitution kit (Ref. AMM TASK 49-10-00-040-007-A01).
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific
AR
CAP - BLANKING
No specific
AR
PLUG - BLANKING
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03QBA1)
Dry lubricant-General Assembly - -
No specific
lockwire-corrosion resistant steel 0.8 mm (0.032 in.) dia.
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
315AL, 316AR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
10
CABLE MOUNT ASSEMBLY
AIPC 49-11-04-05-010
0
APU SUBSTITUTION KIT WITHOUT GENERATOR
AIPC 49-11-04-05-220
3
TRANSVERSE SUPPORT
AIPC 49-11-04-10-010
0
APU SUBSTITUTION KIT
AIPC 49-11-04-10-330
 E. 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 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
TASK 52-41-18-000-001-A
Removal of the APU Exhaust Access-Fairing
TASK 52-41-18-400-001-A
Installation of the APU Exhaust Access-Fairing
3. Job Set-up
Subtask 49-11-00-860-050-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 pushbutton switch is off.
   (3) Make sure that the hydraulic systems are depressurized
(Ref. AMM TASK 29-00-00-864-001).
   (4) Make sure that the APU air intake is closed.
   (5) Make sure that the APU LP fuel valve is closed.
Subtask 49-11-00-010-056-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Put an ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below APU access doors 315AL and 316AR.
   (2) Open APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
   (3) Remove the APU exhaust access-fairing (Ref. AMM TASK 52-41-18-000-001).
   (4) Set LIGHT control switch 11LJ to the ON position.
Subtask 49-11-00-865-057-A ** ON A/C NOT FOR ALL
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAPU/FUEL/BLOW OFF/PUMP2QCB14
121VUAPU/FUEL/BLOW OFF/CTL1QCK39
121VUAPU/FIRE AND OVHT/DET/LOOP B2WGL44
121VUAPU/FIRE AND OVHT/DET/LOOP A1WGL43
121VUAPU/APU/CTL2KDL42
121VUAPU/ECB/SPLY1KDL41
121VUAPU/FIRE/EXTIG/SQUIB/B2WFL39
121VUAPU/FIRE/EXTIG/SQUIB/A1WFL38
121VUAPU/FIRE/LP VALVE/NORM4WFM42
121VUAPU/FIRE/LP VALVE/STBY3WFM41
121VUAPU/FUEL/LP VALVE/CTL1QFM40
121VUAPU/FUEL/LP VALVE/SPLY2QFM39
121VUAPU/FUEL/PUMP/CTL3QCM38
4. Procedure
Subtask 49-11-00-420-056-A ** ON A/C NOT FOR ALL
A. Installation of the APU Substitution Kit
   (1) Install the AIPC 49-11-04-10-010 TRANSVERSE SUPPORT (3) from the AIPC 49-11-04-10-330 APU SUBSTITUTION KIT (0) to the left and right APU mount assemblies with washers (2) and nuts (1).
   (2) Install the
AIPC 49-11-04-05-010 CABLE MOUNT ASSEMBLY (10) of the AIPC 49-11-04-05-220 APU SUBSTITUTION KIT WITHOUT GENERATOR (0) on the transverse support (3) with the bolts (6), the washers (5) and the nuts (4).
   (3) Connect the starter cables (20) to the transverse support (3) with the nuts (21)and the washers (22).
   (4) Connect the generator cables (7) to the cable mount assembly (10) with the nuts (9) and the washers (8).
   (5) Connect the generator control cable (40) to the dummy plug on the cable mount assembly (10).
   (6) Install the CAP - BLANKING (19) on the connector sockets 7120VC, 7118VC and 7138VC, which are on the forward bulkhead FR80.
   (7) Install the rear suspension assembly (18) with the nut (13) to the aft mount assembly (11).
   (8) Install and support the rear suspension assembly (18) with the bolt (14), the washers (16) and the nut (17) to the top bracket (15).
   (9) Before installing the blanking plug to the fuel feed pipe (29), apply Dry lubricant-General Assembly - - (Material No.
03QBA1) to the internal threads.
   (10) Install the PLUG - BLANKING (28) to the APU fuel feed pipe (29).
   (11) Attach the APU fuel feed pipe (29) to the bracket on the bulkhead with lockwire-corrosion resistant steel 0.8 mm (0.032 in.) dia..
   (12) Install the blanking plugs (38) on the APU access door 316AR drain interfaces.
   (13) Install the exhaust muffler plug (32) to the APU exhaust outlet (33).
   (14) Install the blanking plug (27) to the exhaust muffler drain (30).
   (15) Install the bleed-air duct plug (35) to the bleed air duct (24) with the tie-rods (23), the bolts (34), the washers (36) and the nuts (37).
   (16) Install the oil-cooler outlet-duct plug (31) on door 315AL with the screws (26) and the washers (25).
Subtask 49-11-00-865-058-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/FIRE AND OVHT/DET/LOOP B2WGL44
121VUAPU/FIRE AND OVHT/DET/LOOP A1WGL43
121VUAPU/FIRE/EXTIG/SQUIB/B2WFL39
121VUAPU/FIRE/EXTIG/SQUIB/A1WFL38
5. Close-up
Subtask 49-11-00-410-056-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) Set LIGHT control switch 11LJ to the OFF position.
   (3) Close APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-410-001).
   (4) Install the APU exhaust access-fairing (Ref. AMM TASK 52-41-18-400-001).
   (5) Remove the access platform(s).
Subtask 49-11-00-860-063-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Put a warning notice in the cockpit to tell the persons that the APU is not installed.
NOTE: The circuit breakers 1KD, 2KD, 1QC, 2QC, 3QC, 1QF and 2QF must be opened and tagged and must remain so until the APU is reinstalled.
   (2) Make an entry in the aircraft technical log book.
   (3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 01:26:37 UTC