R  EFF : 001-049, 101-105, 107-107, 151-199, 49-42-51Page 209 201-210, Config-2 Aug 01/05
 CES

 (3)
 Put a warning notice in the cockpit to tell persons not to start the APU.

 (4)
 Make sure that hydraulic systems are depressurized
 (Ref. TASK 29-00-00-864-001).

 Subtask 49-42-51-865-071
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD.
 Subtask 49-42-51-010-066
 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. TASK 52-41-00-010-001).

 (3)
 Set the LIGHT control SW 11LJ to the ON position.

 4. Procedure
_________ Subtask 49-42-51-210-059
 A. Inspection of the Starter Motor and Clutch Assembly.
 (1)
 Remove the starter motor (Ref. TASK 49-42-51-000-004).

 (2)
 Do a visual check of the starter motor. Make sure that the external condition of the starter motor is correct.

 (3)
 Do a visual check of the starter motor clutch assembly. Make sure that the internal splines are satisfactory. Replace the clutch assembly if the internal splines have a crack, are broken or missing (Ref. TASK 49-42-52-000-003) (Ref. TASK 49-42-52-400-003).

 (4)
 Do a visual check of the starter motor drive shaft. Make sure that the external splines are satisfactory. Replace the starter motor if the splines are cracked, broken or missing .

 (5)
 Do a visual check of the starter motor/accessory drive gearbox mating faces.

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-42-51Page 210 201-210, Config-2 Aug 01/05
 CES

 (6) Install the starter motor (Ref. TASK 49-42-51-400-004).
 ________

5. Close-up
 Subtask 49-42-51-410-063
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Set the LIGHT control 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 49-42-51-865-072

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

 Subtask 49-42-51-860-070
 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 warning notice(s).

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-42-51Page 211 201-210, Config-2 Aug 01/05
 CES

 TASK 49-42-51-400-004
 Installation of the Starter Motor (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  Torque Wrench : range 0.00 to 1.20 m.daN
 (0.00 to 9.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 03-002  GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
14 packing  49-42-09 01 -030

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-42-51Page 212 201-210, Config-2 Aug 01/05
 CES

 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through the Ground Connector 49-42-52-000-003 Removal of the Starter Motor Clutch (8033KM) (131-9(A)) 49-42-52-400-003 Installation of Starter Motor Clutch (8033KM)
　
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 POWER4(102)