CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ 201-210, Surge Control Valve (SCV) 7 001-049, 101-105 107-107, 151-199 201-210, Load Control Valve 9 001-049, 101-105 107-107, 151-199 201-210, Operation/Control and Indication 9 001-049, 101-105 107-107, 151-199 201-210, Start Procedure of APU Bleed-Air 9 001-049, 101-105 Supply 107-107, 151-199 201-210, Stop of the APU Bleed-Air Supply 10 001-049, 101-105 107-107, 151-199 201-210, Indicating 10 001-049, 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 Primary Components 1 106-106, 108-149 211-299, 301-399 Bleed and Surge Air System 1 106-106, 108-149 211-299, 301-399 Interface 4 106-106, 108-149 211-299, 301-399 Component Description 4 106-106, 108-149 211-299, 301-399 Bleed Control Valve (BCV) 4 106-106, 108-149 211-299, 301-399 Compressor Discharge 4 106-106, 108-149 Pressure-Sensors 211-299, 301-399 Compressor Discharge Pressure 4 106-106, 108-149 Sensor 211-299, 301-399 Operation/Control and Indication 6 106-106, 108-149 211-299, 301-399 Start Procedure of APU Bleed-Air 6 106-106, 108-149 Supply 211-299, 301-399 Indicating 9 106-106, 108-149
49-CONTENTS Page 56 Aug 01/05 R CES
CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ 211-299, 301-399
BLEED AND SURGE AIR 49-51-00
DEACTIVATION/REACTIVATION 1 401 051-099, 401-499 Deactivation of the APU Bleed Load 401 001-003, 051-099 Control-Valve (8050KM) (GTCP 401-499, 36-300)
Refer to the MMEL TASK: 36-12-02 401 001-003, 051-099
401-499, Reactivation of the APU Bleed Load 406 001-003, 051-099 Control-Valve (8050KM) (GTCP 401-499, 36-300)
Refer to the MMEL TASK: 36-12-02 406 001-003, 051-099 401-499,
DEACTIVATION/REACTIVATION 2 401 001-049, 101-105 107-107, 151-199 201-210,
Deactivation of the APU Load 401 001-049, 101-105 Control-Valve (131-9(A)) 107-107, 151-199 201-210,
Refer to the MMEL TASK: 36-12-02 401 001-049, 101-105 107-107, 151-199 201-210,
Reactivation of the APU Load 406 001-049, 101-105 Control-Valve (131-9(A)) 107-107, 151-199 201-210,
Refer to the MMEL TASK: 36-12-02 406 001-049, 101-105 107-107, 151-199 201-210,
DEACTIVATION/REACTIVATION 3 401 106-106, 108-149
211-299, 301-399 Deactivation of the Bleed Control 401 106-106, 108-149 Valve (8051KM) (APS 3200) 211-299, 301-399
Refer to the MMEL TASK: 36-12-02 401 106-106, 108-149
211-299, 301-399 Reactivation of the Bleed Control 406 106-106, 108-149 Valve (8051KM) (APS 3200) 211-299, 301-399
Refer to the MMEL TASK: 36-12-02 406 106-106, 108-149 211-299, 301-399 SENSOR ASSY - PNEUMATIC 49-51-13
REMOVAL/INSTALLATION 401 051-099, 401-499 Removal of the Pneumatic Sensor 401 001-003, 051-099 Assy (GTCP 36-300) 401-499, Installation of the Pneumatic 405 001-003, 051-099 Sensor Assy (GTCP 36-300) 401-499,
49-CONTENTS Page 57 Aug 01/05 R CES
CHAPTER 49
__________
AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ SENSOR - TOTAL PRESSURE 49-51-14 REMOVAL/INSTALLATION 401 051-099, 401-499 Removal of the Airflow Sensor 401 001-003, 051-099 (GTCP 36-300) 401-499, Installation of the Airflow Sensor 406 001-003, 051-099 (GTCP 36-300) 401-499,
TRANSDUCER - DIFFERENTIAL PRESSURE 49-51-16
REMOVAL/INSTALLATION 1 401 051-099, 401-499 Removal of the Differential 401 001-003, 051-099 Pressure Transducer (8043KM) (GTCP 401-499, 36-300) Installation of the Differential 405 001-003, 051-099 Pressure Transducer (8043KM) (GTCP 401-499, 36-300)
REMOVAL/INSTALLATION 2 401 001-049, 101-105 107-107, 151-199 201-210,
Removal of the Transducer -401 001-049, 101-105 Differential Pressure (8043KM) 107-107, 151-199 (131-9(A)) 201-210, Installation of the Transducer -405 001-049, 101-105 Differential Pressure (8043KM) 107-107, 151-199 (131-9(A)) 201-210,
TRANSDUCER - TOTAL PRESSURE 49-51-17
REMOVAL/INSTALLATION 1 401 051-099, 401-499 Removal of the Total Pressure 401 001-003, 051-099 Sensor (8044KM) (GTCP 36-300) 401-499, Installation of the Total Pressure 405 001-003, 051-099 Sensor (8044KM) (GTCP 36-300) 401-499,
REMOVAL/INSTALLATION 2 401 001-049, 101-105 107-107, 151-199 201-210,
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 機(jī)載輔助動(dòng)力 AIRBORNE AUXILIARY POWER1(63)
