(9)
Remove the starter cables (20) from the cross member assembly (3) and attach them temporarily to the bulkhead.
(10)
Support the cross member assembly (3) and remove the nuts (1) the washers (2) and fit the thread protectors.
(11)
Remove the blanking plug (28) from the APU fuel feed pipe (29).
(12)
Remove the blanking caps (19) from the connector sockets 7120VC, 7138VC and 7118VC.
(13)
Remove the cross member assembly (3). Subtask 49-11-00-420-059
B.
Install the APU. (Ref. TASK 49-11-11-400-004)
5. Close-up
________ Subtask 49-11-00-410-062
A. Close Access
(1)
Set the LIGHT SW 11LJ to the OFF position.
(2)
Close the APU access doors 315AL, 316AR and (Ref. TASK 52-41-00-410-001).
(3)
Close the APU exhaust access fairing 317.
(4)
Remove the access platform(s).
R EFF : 001-049, 101-105, 107-107, 151-199, 49-11-00Page 810 201-210, Config-2 Aug 01/05
CES Subtask 49-11-00-860-068
B. 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, 49-11-00Page 811 201-210, Config-2 Aug 01/05
CES TASK 49-11-00-400-006
Installation of the Generator Substitution Kit (Flight without Generator) (131-9(A))
WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS
_______ WHEN YOU DO THE MAINTENANCE TASK(S).
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform 3.5 m (11 ft. 6 in.)
No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00
to 75.00 lbf.ft) 3862619-1 1 COVER - ASSEMBLY, APU GEN
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. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
R EFF : 001-049, 101-105, 107-107, 151-199, 49-11-00Page 812 201-210, Config-2 Aug 01/05
CES
C. 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 49-00-00-860-008 APU Start by External Power (131-9(A)) 49-00-00-860-009 APU Shutdown by External Power (131-9(A)) 49-90-00-600-007 Check and Replenish Oil Level (131-9(A)) 52-41-00-010-001 Open the APU Doors for Access 52-41-00-410-001 Close the APU Doors after Access AIPC 49110405010 49-11-00-991-009 Fig. 803
3. Job Set-up
__________
Subtask 49-11-00-860-069
A. Aircraft Maintenance Configuration
(1)
Energize the ground service network
(Ref. TASK 24-42-00-861-001).
(2)
On the panel 25VU make sure that the APU MASTER SW p/bsw is OFF.
(3)
Make sure that hydraulic systems are depressurized
(Ref. TASK 29-00-00-864-001).
Subtask 49-11-00-865-067
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
R EFF : 001-049, 101-105, 107-107, 151-199, 49-11-00Page 813 201-210, Config-2 Aug 01/05 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER2(8)
