• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 14:32来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 2.
 Component Location


__________________
 (Ref. Fig. 001)

 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
 | | | | DOOR | REF. -------------------------------------------------------------------------------4005KM AUXILIARY POWER UNIT 315/ 315AL/ 49-11-11
 316 316AR
 3. System Description
__________________
 The APU consists of the following subsystems:

 -APU Mounts (Ref. 49-12-00)
 -Air Intake System (Ref. 49-16-00)
 -Power Plant Drain System (Ref. 49-17-00)
 -
Engine (Ref. 49-20-00)

 -
Engine Fuel and Control (Ref. 49-30-00)


 -Ignition and Starting (Ref. 49-40-00)
 -Air (Ref. 49-50-00)
 -Engine Controls (Ref. 49-60-00)
 -Indicating (Ref. 49-70-00)
 -Oil (Ref. 49-90-00)


 Power Plant Installation - Component Location
 Figure 001

 CES  POWER PLANT - DESCRIPTION AND OPERATION


_______________________________________
 1.
 General

_______ The central component of the power plant is the APU. It is installed in a fireproof compartment between FR80 and FR84. The access doors 315AL and 316AR (Ref. 52-42-00), which together are the lower compartment wall, permit installation, servicing and removal of the APU.

 2.
 Component Location


__________________
 (Ref. Fig. 001)

 -------------------------------------------------------------------------------
FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
 | | | | DOOR | REF. -------------------------------------------------------------------------------4005KM AUXILIARY POWER UNIT 315/ 315AL/ 49-11-11
 316 316AR
 3. System Description
__________________
 The APU consists of the following subsystems:

 -APU Mounts (Ref. 49-12-00)
 -Air Intake System (Ref. 49-16-00)
 -Power Plant Drain System (Ref. 49-17-00)
 -
Engine (Ref. 49-20-00)

 -
Engine Fuel and Control (Ref. 49-30-00)


 -Ignition and Starting (Ref. 49-40-00)
 -Air (Ref. 49-50-00)
 -Engine Controls (Ref. 49-60-00)
 -Indicating (Ref. 49-70-00)
 -Exhaust (Ref. 49-80-00)
 -Oil (Ref. 49-90-00)

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-11-00Page 1 201-210, Config-2 Aug 01/05
 CES


 Power Plant - Component Location
 Figure 001

 CES  POWER PLANT - DESCRIPTION AND OPERATION


_______________________________________
 1.
 General

_______ The central component of the power plant is the APU. It is installed in a fireproof compartment between FR80 and FR84 (Ref. 53-58-00). The access doors 315AL and 316AR (Ref. 52-42-00), which together are the lower compartment wall, permit installation, servicing and removal of the APU.

 2.
 Component Location


__________________
 (Ref. Fig. 001)

 -------------------------------------------------------------------------------
FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
 | | | | DOOR | REF. -------------------------------------------------------------------------------4005KM AUXILIARY POWER UNIT 315/ 315AL/ 49-11-11
 316 316AR
 3. System Description
__________________
 The APU consists of the following subsystems:

 -APU Mounts (Ref. 49-12-00)
 -Air Intake System (Ref. 49-16-00)
 -Power Plant Drain System (Ref. 49-17-00)
 -
Engine (Ref. 49-20-00)

 -
Engine Fuel and Control (Ref. 49-30-00)


 -Ignition and Starting (Ref. 49-40-00)
 -Air (Ref. 49-50-00)
 -Engine Controls (Ref. 49-60-00)
 -Indicating (Ref. 49-70-00)
 -Oil (Ref. 49-90-00)


 Power Plant Installation - Component Location
 Figure 001

 CES


 POWER PLANT ((GTCP 36-300)) - REPAIRS
_____________________________________

R **ON A/C 001-003, 051-099, 401-499,
 TASK 49-11-00-400-001
 Installation of the APU Substitution Kit (GTCP 36-300)

 1.
 Reason for the Job

__________________
 APU removed, replacement APU not available.


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
 
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 POWER1(157)