CHAPTER 49
__________
 AIRBORNE AUXILIARY POWER
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ 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, Component Description 1 001-049, 101-105 107-107, 151-199 201-210, Fuel Control Unit 1 001-049, 101-105 107-107, 151-199 201-210, Operation/Control and Indication 3 001-049, 101-105 107-107, 151-199 201-210, APU Fuel System 3 001-049, 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 Fuel Control Unit (FCU) 1 106-106, 108-149 211-299, 301-399 Flow Divider 3 106-106, 108-149 211-299, 301-399 Operation/Control and Indication 3 106-106, 108-149 211-299, 301-399 APU Fuel System 3 106-106, 108-149 211-299, 301-399
 APU FUEL CONTROL ((APS 3200)) 49-32-00 INSPECTION/CHECK 2 601 106-106, 108-149
 211-299, 301-399 Visual Check of Fuel Distribution 601 106-106, 108-149 System for Condition and Security 211-299, 301-399 (APS 3200)
 CONTROL UNIT - FUEL ((GTCP 36-300)) 49-32-11
 SERVICING 1 301 051-099, 401-499 Inspection of the Fuel-Filter 301 001-003, 051-099 Differential-Pressure Indicator 401-499,
 49-CONTENTS Page 43 Aug 01/05 R CES

 CHAPTER 49
__________
 AIRBORNE AUXILIARY POWER
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ (GTCP 36-300) Servicing of the Fuel Filter (GTCP 305 001-003, 051-099 36-300) 401-499, CONTROL UNIT - FUEL ((APS 3200)) 49-32-11 SERVICING 2 301 106-106, 108-149 211-299, 301-399 Differential Pressure Indicator -301 106-106, 108-149 Inspection/Check (APS 3200) 211-299, 301-399 Fuel Filter Element -305 106-106, 108-149 Removal/Installation (APS 3200) 211-299, 301-399
 CONTROL UNIT - FUEL  49-32-11
 REMOVAL/INSTALLATION 1 401 051-099, 401-499 Removal of the Fuel Control Unit 401 001-003, 051-099 (FCU) (8022KM) (GTCP 36-300) 401-499, Installation of the Fuel Control 406 001-003, 051-099 Unit (FCU) (8022KM) (GTCP 36-300) 401-499,
 REMOVAL/INSTALLATION 2 401  001-049, 101-105 107-107, 151-199 201-210,
 Removal of the Fuel Control Unit 401 001-049, 101-105 (FCU) (8022KM) (131-9(A)) 107-107, 151-199
 201-210, Installation of the Fuel Control 405 001-049, 101-105 Unit (FCU) (8022KM) (131-9(A)) 107-107, 151-199
 201-210, REMOVAL/INSTALLATION 3 401 106-106, 108-149
 211-299, 301-399 Removal of the Fuel Control Unit 401 106-106, 108-149 (8022KM) (APS 3200) 211-299, 301-399 Installation of the Fuel Control 405 106-106, 108-149 Unit (8022KM) (APS 3200) 211-299, 301-399
 FLOW DIVIDER AND DRAIN VALVE ASSY 49-32-12
 REMOVAL/INSTALLATION 1 401 051-099, 401-499 Removal of the Flow Divider and 401 001-003, 051-099 Drain Valve Assembly (8023KM) 401-499, (GTCP 36-300) Installation of the Flow Divider 405 001-003, 051-099 and Drain Valve Assembly (8023KM) 401-499, (GTCP 36-300)
 REMOVAL/INSTALLATION 2 401  106-106, 108-149
 211-299, 301-399 Removal of the Flow Divider 401 106-106, 108-149 (8024KM) (APS 3200) 211-299, 301-399 Installation of the Flow Divider 405 106-106, 108-149 (8024KM) (APS 3200) 211-299, 301-399
 FLOW DIVIDER  49-32-13
 49-CONTENTS Page 44 Aug 01/05 R CES

 CHAPTER 49
__________
 AIRBORNE AUXILIARY POWER
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ REMOVAL/INSTALLATION 401 001-049, 101-105 107-107, 151-199 201-210, Removal of Flow Divider and 401 001-049, 101-105 Solenoid Valve (8024KM) (131-9(A)) 107-107, 151-199 201-210, Installation of Flow Divider and 405 001-049, 101-105 Solenoid Valve (8024KM) (131-9(A)) 107-107, 151-199 201-210, SOLENOID VALVE - APU FUEL SHUTOFF 49-32-17 REMOVAL/INSTALLATION 401 051-099, 401-499 Removal of the Fuel Shutoff 401 001-003, 051-099 Solenoid-Valve (8026KM) (GTCP 401-499, 36-300) Installation of the Fuel Shutoff 405 001-003, 051-099 Solenoid-Valve (8026KM) (GTCP 401-499, 36-300) FILTER - FUEL ((131-9(A))) 49-32-41 MAINTENANCE PRACTICES 1 201 001-049, 101-105 107-107, 151-199 201-210, Replacement of the Fuel Filter 201 001-049, 101-105 (8028KM) (131-9(A)) 107-107, 151-199 201-210, FILTER - FUEL 49-32-41 MAINTENANCE PRACTICES 2 201 106-106, 108-149 211-299, 301-399 Replacement of the Fuel Filter 201 106-106, 108-149 (8028KM) (APS 3200) 211-299, 301-399 VALVE - DRAIN, COMBUSTION CHAMBER 49-32-51 REMOVAL/INSTALLATION 401 106-106, 108-149 211-299, 301-399 Removal of the Combustion Chamber 401 106-106, 108-149 Drain Valve (APS 3200) 211-299, 301-399 Installation of the Combustion 405 106-106, 108-149 Chamber Drain Valve (APS 3200) 211-299, 301-399
　
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(59)