CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ STARTING State 7 106-106, 108-149 211-299, 301-399 RUN State 7 106-106, 108-149 211-299, 301-399 COOLDOWN State 7 106-106, 108-149 211-299, 301-399 SHUTDOWN State 7 106-106, 108-149 211-299, 301-399 Display 25 106-106, 108-149 211-299, 301-399 Normal Mode 25 106-106, 108-149 211-299, 301-399 Menu Mode 25 106-106, 108-149 211-299, 301-399 AIDS 33 106-106, 108-149 211-299, 301-399 MES/IDLE Report 33 106-106, 108-149 211-299, 301-399 SHUTDOWN Report 33 106-106, 108-149 211-299, 301-399 BITE Test 35 106-106, 108-149 211-299, 301-399 Power-up Test 35 106-106, 108-149 211-299, 301-399 Manually Initiated Test 36 106-106, 108-149 211-299, 301-399 Linear Voltage Differential 36 106-106, 108-149 Tranducer (LVDT) compensation 211-299, 301-399 Fault Detection 36 106-106, 108-149 211-299, 301-399 ENGINE IDENTIFICATION MODULE 49-73-31 REMOVAL/INSTALLATION 401 106-106, 108-149 211-299, 301-399 Engine Identification Module 401 106-106, 108-149 (8061KM) - Removal (APS 3200) 211-299, 301-399 Engine Identification Module 405 106-106, 108-149 (8061KM) - Installation (APS 3200) 211-299, 301-399 DATA MEMORY MODULE 49-73-32 REMOVAL/INSTALLATION 401 001-049, 101-105 107-107, 151-199 201-210, Removal of the Data Memory Module 401 001-049, 101-105 (8062KM) (131-9(A)) 107-107, 151-199 201-210, Installation of the Data Memory 405 001-049, 101-105 Module (8062KM) (131-9(A)) 107-107, 151-199
49-CONTENTS Page 80 Aug 01/05 R CES
CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ 201-210, ENCODER 49-73-51 REMOVAL/INSTALLATION 401 051-099, 401-499 Removal of the Encoder (8063KM) 401 001-003, 051-099 (GTCP 36-300) 401-499, Installation of the Encoder 405 001-003, 051-099 (8063KM) (GTCP 36-300) 401-499,
EXHAUST 49-80-00
_______ DESCRIPTION AND OPERATION 1 1 051-099, 401-499 General 1 001-003, 051-099 401-499, Component Location 1 001-003, 051-099 401-499, System Description 1 001-003, 051-099 401-499, Muffler Assembly (Ref. 49-81-00) 1 001-003, 051-099 401-499, Access Fairing Seal (Ref. 1 001-003, 051-099 52-41-18) 401-499, DESCRIPTION AND OPERATION 2 1 001-049, 101-105 107-107, 151-199 201-210, General 1 001-049, 101-105 107-107, 151-199 201-210, System Description 1 001-049, 101-105 107-107, 151-199 201-210, Muffler Assembly (Ref. 49-81-00) 1 001-049, 101-105 107-107, 151-199 201-210, Access Fairing Seal (Ref. 1 001-049, 101-105 52-41-18) 107-107, 151-199 201-210, DESCRIPTION AND OPERATION 3 1 106-106, 108-149 211-299, 301-399 General 1 106-106, 108-149 211-299, 301-399 Component Location 1 106-106, 108-149 211-299, 301-399 System Description 1 106-106, 108-149 211-299, 301-399 Muffler Assembly (Ref. 49-81-00) 1 106-106, 108-149 211-299, 301-399 Access Fairing Seal (Ref. 1 106-106, 108-149
49-CONTENTS Page 81 Aug 01/05 R CES
CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ 52-41-18) 211-299, 301-399
EXHAUST SYSTEM 49-81-00 DESCRIPTION AND OPERATION 1 1 051-099, 401-499 General 1 001-003, 051-099 401-499, Component Location 1 001-003, 051-099 401-499, System/Component Description 4 001-003, 051-099 401-499, Major Components 4 001-003, 051-099 401-499, Muffler Assembly Installation 5 001-003, 051-099 401-499, Operation 5 001-003, 051-099 401-499, DESCRIPTION AND OPERATION 2 1 001-049, 101-105 107-107, 151-199 201-210, General 1 001-049, 101-105 107-107, 151-199 201-210, Component Location 1 001-049, 101-105 107-107, 151-199 201-210, System/Component Description 4 001-049, 101-105 107-107, 151-199 201-210, Major Components 4 001-049, 101-105 107-107, 151-199 201-210, Muffler Assembly Installation 5 001-049, 101-105 107-107, 151-199 201-210, Operation 5 001-049, 101-105 107-107, 151-199 201-210, DESCRIPTION AND OPERATION 3 1 106-106, 108-149 211-299, 301-399 General 1 106-106, 108-149 211-299, 301-399 Component Location 1 106-106, 108-149 211-299, 301-399 System/Component Description 4 106-106, 108-149 211-299, 301-399 Major Components 4 106-106, 108-149
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(71)
