B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-23-51-400-001 Installation of the APU Generator 8XS 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 52-41-00-410-001 Close the APU Doors after Access AIPC 49110405010 49-11-00-991-009 Fig. 803
R EFF : 001-049, 101-105, 107-107, 151-199, 49-11-00Page 818 201-210, Config-2 Aug 01/05
CES 3. Job Set-up
__________ Subtask 49-11-00-860-071
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 pushbutton switch is off.
(3)
Make sure that hydraulic systems are depressurized
(Ref. TASK 29-00-00-864-001).
(4)
Put a container below the cover assembly (3) to collect the oil which will flow when you remove the drain plug (5).
Subtask 49-11-00-865-069
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 49-11-00-010-063
C. Get Access
(1)
Put the access platform in position below the APU compartment.
(2)
Open the APU access doors 315AL, 316AR.
(3)
Set the LIGHT switch to the ON position.
R EFF : 001-049, 101-105, 107-107, 151-199, 49-11-00Page 819 201-210, Config-2 Aug 01/05
CES 4. Procedure
_________ Subtask 49-11-00-020-061
A. Removal of the Generator Substitution Kit (131-9(A))
(Ref. Fig. 803/TASK 49-11-00-991-009)
(1) Put a container below the cover assembly (3) to collect the oil which will flow when you remove the drain plug (5).
WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO
_______ PREVENT BURNS WHEN YOU DO THE MAINTENANCE TASK(S).
(2)
Remove and discard the lockwire from the drain plug (5).
(3)
Remove the drain plug (5) from the cover assembly (3).
(4)
Remove the electrical connector (7) and the electrical cable connections (9) from the generator cable support (6).
(5)
Put blanking caps on the disconnected electrical connectors.
(6)
Remove the nuts (4) from the cover assembly (3) and from the generator cable support (6).
(7)
Remove the COVER - ASSEMBLY, APU GEN (3) and the generator cable support (6) (Ref. AIPC 49110405010) from the mounting flange (1).
(8)
Do an inspection of the component interface and/or the adjacent area.
(9)
Clean the component interface and/or the adjacent area.
(10) Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 49-11-00-420-061
B. Install the APU generator 8XS to the mounting flange (1) (Ref. TASK 24-23-51-400-001).
R EFF : 001-049, 101-105, 107-107, 151-199, 49-11-00Page 820 201-210, Config-2 Aug 01/05
CES 5. Close-up
________ Subtask 49-11-00-410-064
A. Close Access
(1)
Set the LIGHT SW to the Off position.
(2)
Close the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-410-001).
(3)
Remove the access platform(s). Subtask 49-11-00-860-072
B.
Aircraft Maintenance Configuration
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(10)
