REMOVAL/INSTALLATION 401 051-099, 401-499 Removal of the Compressor 401 001-003, 051-099 Inlet-Pressure Sensor (GTCP 401-499, 36-300) Installation of the Compressor 405 001-003, 051-099 Inlet-Pressure Sensor (GTCP 401-499, 36-300)
49-CONTENTS Page 58 Aug 01/05 R CES
CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ PROBE - TOTAL PRESSURE 49-51-19 REMOVAL/INSTALLATION 1 401 001-049, 101-105 107-107, 151-199 201-210, Removal of the Probe - Total 401 001-049, 101-105 Pressure (131-9(A)) 107-107, 151-199 201-210, Installation of the Probe - Total 405 001-049, 101-105 Pressure (131-9(A)) 107-107, 151-199 201-210, SENSOR - COMPRESSOR DISCHARGE PRESSURE 49-51-19 REMOVAL/INSTALLATION 2 401 106-106, 108-149 211-299, 301-399 Removal of the Sensor - Compressor 401 106-106, 108-149 Discharge Pressure (8039KM) (APS 211-299, 301-399 3200) Installation of the Sensor -405 106-106, 108-149 Compressor Discharge Pressure 211-299, 301-399 (8039KM) (APS 3200) TRANSDUCER - APU INLET PRESSURE 49-51-21 REMOVAL/INSTALLATION 401 001-049, 101-105 107-107, 151-199 201-210, Removal of the Transducer - APU 401 001-049, 101-105 Inlet Pressure (8048KM) (131-9(A)) 107-107, 151-199 201-210, Installation of the Transducer -404 001-049, 101-105 APU Inlet Pressure (8048KM) 107-107, 151-199 (131-9(A)) 201-210, DUCT - BLEED AIR 49-51-42 REMOVAL/INSTALLATION 1 401 051-099, 401-499 Removal of the Surge/Bleed Duct 401 001-003, 051-099 (8049KM) (GTCP 36-300) 401-499, Installation of the Surge/Bleed 406 001-003, 051-099 Duct (8049KM) (GTCP 36-300) 401-499, Installation of the Sensor 411 001-003, 051-099 Assembly (GTCP 36-300) 401-499, DUCT - AIR BYPASS 49-51-42 REMOVAL/INSTALLATION 2 401 106-106, 108-149 211-299, 301-399 Air By-Pass Duct - Removal (APS 401 106-106, 108-149 3200) 211-299, 301-399 Air By-Pass Duct - Installation 405 106-106, 108-149 (APS 3200) 211-299, 301-399 VALVE - LOAD CONTROL 49-51-51 REMOVAL/INSTALLATION 1 401 051-099, 401-499
49-CONTENTS Page 59 Aug 01/05 R CES
CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Removal of the Bleed Load 401 001-003, 051-099 Control-Valve (8050KM) (GTCP 401-499, 36-300) Installation of the Bleed Load 405 001-003, 051-099 Control-Valve (8050KM) (GTCP 401-499, 36-300) REMOVAL/INSTALLATION 2 401 001-049, 101-105 107-107, 151-199 201-210, Removal of the Load Control Valve 401 001-049, 101-105 (8050KM) (131-9(A)) 107-107, 151-199 201-210, Installation of the Load Control 405 001-049, 101-105 Valve (8050KM) (131-9(A)) 107-107, 151-199 201-210, VALVE - SURGE CONTROL ((GTCP 36-300)) 49-51-52 SERVICING 301 051-099, 401-499 Clean Surge Valve Filter (GTCP 301 001-003, 051-099 36-300) 401-499, VALVE - SURGE CONTROL 49-51-52 REMOVAL/INSTALLATION 1 401 051-099, 401-499 Removal of the Surge Control Valve 401 001-003, 051-099 (8058KM) (GTCP 36-300) 401-499, Installation of the Surge Control 405 001-003, 051-099 Valve (8058KM) (GTCP 36-300) 401-499, REMOVAL/INSTALLATION 2 401 001-049, 101-105 107-107, 151-199 201-210, Removal of the Surge Control Valve 401 001-049, 101-105 (8058KM) (131-9(A)) 107-107, 151-199 201-210, Installation of the Surge Control 405 001-049, 101-105 Valve (8058KM) (131-9(A)) 107-107, 151-199 201-210, VALVE - BLEED CONTROL 49-51-53 REMOVAL/INSTALLATION 401 106-106, 108-149 211-299, 301-399 Removal of the Bleed Control Valve 401 106-106, 108-149 (8051KM) (APS 3200) 211-299, 301-399 Installation of the Bleed Control 407 106-106, 108-149 Valve (8051KM) (APS 3200) 211-299, 301-399 BYPASS VALVE 49-51-54 REMOVAL/INSTALLATION 401 059-099, 401-499 Removal of the Buffer-Air Bypass 401 059-099, 401-499 Valve (GTCP 36-300) Installation of the Buffer-Air 404 059-099, 401-499
49-CONTENTS Page 60 Aug 01/05 R CES
CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Bypass Valve (GTCP 36-300)
ACCESSORY COOLING 49-52-00 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, Cooling Fan 1 001-003, 051-099 401-499, Oil-Cooler Cooling Air 4 001-003, 051-099 401-499, APU Compartment Cooling Air 4 001-003, 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 Description 1 001-049, 101-105 107-107, 151-199 201-210, Cooling Fan 1 001-049, 101-105 107-107, 151-199 201-210, Oil-Cooler Cooling Air 4 001-049, 101-105 107-107, 151-199 201-210, APU Compartment Cooling Air 4 001-049, 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 Description 1 106-106, 108-149 211-299, 301-399 Cooling Fan 1 106-106, 108-149
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 POWER1(64)
