5. Close-up
________ Subtask 49-11-00-410-059
A. Close Access
(1)
Set the LIGHT switch to the Off position.
(2)
Close the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-410-001).
(3)
Close the APU exhaust access fairing 317.
(4)
Remove the access platform(s). Subtask 49-11-00-860-062
B.
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
POWER PLANT - MAINTENANCE PRACTICES
___________________________________
TASK 49-11-11-400-005
Build-up of the APU (131-9(A))
1. Reason for the Job
__________________
This Task gives the APU build-up of the APU (131-9(A)) ready for
installation in the aircraft.
NOTE : Items under paragraph 2.C. Expendable Parts include all items
____
necessary for the APU build-up, not only expendable parts.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00
to 75.00 lbf.ft) FRDH141 1 ADAPTER - TORQUE 98D49207527000 1 SUPPORT FRAME - APU
B.
Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 03-002 GB DEF-STAN 91-101
LUBRICATING OIL TURBINE ENGINE SYNT BASE
(Ref. 20-31-00) Material No. 07-020 AI TNA 007-10012
IDENTIFICATION PAINT (Ref. 20-31-00) Material No. 07-560
SECURING LACQUER (Ref. 20-31-00) Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
R EFF : 001-049, 101-105, 107-107, 151-199, 49-11-11Page 201 201-210, Config-1 Aug 01/05
CES
-------------------------------------------------------------------------------
REFERENCE ------------------------ DESIGNATION-------------------------------------------------------
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
0 Auxiliary Power Unit
1 bolts
2 rear APU mount bracket
3 FWD APU mount bracket (LH)
4 washer
5 nut
7 nut
8 setscrew
9 FWD APU mount bracket (RH)
21 generator
21 generator
21 generator
21 generator
22 preformed packing
22 preformed packing
22 preformed packing
22 preformed packing
23 seal plate
24 nuts
25 seal
25 seal
25 seal
25 seal
26 countersunk screws
49-11-09 01 -00149-11-09 01 -07049-11-09 01 -06049-11-09 01 -04049-11-09 01 -10049-11-09 01 -12049-11-09 01 -11049-11-09 01 -09049-11-09 01 -05024-23-04 01 -010B24-23-04 01 -010C24-23-04 01 -010D24-23-04 01 -010E24-23-04 01 -010B24-23-04 01 -010C24-23-04 01 -010D24-23-04 01 -010E24-23-04 01 -04024-23-04 01 -020A24-23-04 01 -010B24-23-04 01 -010C24-23-04 01 -010D24-23-04 01 -010E24-23-04 01 -030
CES
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-11-11-400-004 Installation of the Power Plant (APU) (131-9(A)) 49-11-11-991-020 Fig. 201 49-11-11-991-013 Fig. 202 49-11-11-991-014 Fig. 203
3. Job Set-up
__________ Subtask 49-11-11-941-053
A. Preparation for Build-up
(1)
Remove the Auxiliary Power Unit (0) from the transport container.
(2)
Install the APU on the SUPPORT FRAME - APU (98D49207527000). (Ref. Fig. 201/TASK 49-11-11-991-020)
中國航空網 m.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(16)
