D. Apply a thin layer of SPECIAL MATERIALS (Material No. 05-027) to the vibration isolator (15), the tie-rod ends, the suspension structural brackets and the APU mount-bracket.
 5. Close-up
________ Subtask 49-12-52-410-052
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Set the LIGHT SW 11LJ to the OFF position.

 (3)
 Close the APU access doors 316AR, 315AL (Ref. TASK 52-41-00-410-001) .

 (4)
 Remove the access platform(s). Subtask 49-12-52-865-059

 B.
 Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD.

 Subtask 49-12-52-860-058
 C. Aircraft Maintenance Configuration
 (1)
 Pressurize the reservoirs of the hydraulic systems.
 (Ref. TASK 29-14-00-614-002).

 (2)
 De-energize the ground service network
 (Ref. TASK 24-42-00-862-001).

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 (4)
 Remove the warning notice(s).

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-12-52Page 414 201-210, Config-2 Aug 01/05
 CES

 VIBRATION ISOLATOR - FWD R (4045KM) - REMOVAL/INSTALLATION
__________________________________________________________ TASK 49-12-52-000-002 Removal of the FWD RH Tie-Rods and Vibration Isolator 4045KM (APS 3200) WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS
_______ WHEN YOU DO THE MAINTENANCE TASK(S).
 WARNING : LOCK THE MECHANISM OF THE ACCESS DOOR 316AR WITH THE PIP PIN WHEN YOU
_______ OPEN THE ACCESS DOOR. THIS WILL PREVENT INJURY.
 CAUTION : DO NOT REMOVE MORE THAN ONE APU MOUNT AT A TIME WHEN THE APU IS
_______ INSTALLED. THE APU HOIST AND THE REMAINING TWO MOUNTS MUST SUPPORT THE APU WHEN YOU REMOVE AN APU MOUNT.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific access platform 3.0 m (9 ft. 10 in.)
 A1-91-265 1 HOIST - MINILIFT
 98A49107504001 1 PROTECTOR - THREADS, APU MOUNTING BOLTS

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action 49-00-00-480-001 Installation of the APU Hoist Tool (APS 3200) 52-41-00-010-001 Open the APU Doors for Access 52-41-21-000-001 Removal of the APU Access Door 315AL 52-41-22-000-001 Removal of the APU Access Door 316AR and the related
 Door Mechanism 49-12-52-991-002 Fig. 401
 3. Job Set-up
__________
 Subtask 49-12-52-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Put the warning notices on panel 25VU to tell persons not to start the APU.

 (2)
 Energize the ground service network (Ref. TASK 24-41-00-861-002).

 (3)
 Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).

 Subtask 49-12-52-865-054
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41

 Subtask 49-12-52-010-051
 C. Get Access
 (1)
 Put the access platform below the access doors 315AL and 316AR.

 (2)
 Open the APU access doors 315AL, 316AR. (Ref. TASK 52-41-00-010-001)

 (3)
 Set the light switch 11LJ to on.

 (4)
 Remove the APU access doors 315AL, 316AR (Ref. TASK 52-41-21-000-001) (Ref. TASK 52-41-22-000-001).

 4. Procedure
_________ (Ref. Fig. 401/TASK 49-12-52-991-002) Subtask 49-12-52-480-051
 A. Installation of the HOIST- MINILIFT
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 機載輔助動力 AIRBORNE AUXILIARY POWER2(97)