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时间:2011-03-22 06:45来源:蓝天飞行翻译 作者:admin
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 Installation of the APU Fuel 406 ALL
 Low-Pressure Valve (14QM)

 ACTUATOR - APU FUEL LP VALVE 28-29-51
 REMOVAL/INSTALLATION 401 ALL
 Removal of the APU Fuel LP Valve 401 ALL

 28-CONTENTS Page 29 Aug 01/05 R CES


 CHAPTER 28
__________
 FUEL
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Actuator (3QF) Installation of the APU Fuel LP 406 ALL Valve Actuator (3QF)
 INDICATING 28-40-00
__________
 DESCRIPTION AND OPERATION 1 ALL
 General 1 ALL
 Component Location 1 ALL
 System Description 1 ALL

 Quantity Indicating (Ref. 1 ALL
 28-42-00)
 Magnetic Level Indicators (Ref. 4 ALL
 28-43-00)
 Fuel Level Sensing System (FLSS) 5 ALL
 (Ref. 28-46-00)

 Power Supply 5 ALL
 Interfaces 7 ALL
 Operation/Control and Indicating 7 ALL

 Control and Indicating 14 ALL
 BITE Test 15 ALL

 INDICATING 28-40-00
___________
 DEACTIVATION/REACTIVATION 401 ALL
 APU LP Valve Indication - Valve 401 ALL
 Closure Procedure

 Refer to the MMEL TASK: 401 ALL
 28-40-06-C)
 Reactivation of the APU LP Valve 404 ALL
 Indication

 Refer to the MMEL TASK: 404 ALL
 28-40-06-C)
 Crossfeed Valve Indication - Valve 407 ALL
 Operating Procedure

 Refer to the MMEL TASK: 407 ALL
 28-40-06-D) Check of the Fuel Quantity 413 001-049, 051-099 Indicating System, When an Outer 101-149, 151-199 Cell Indication is Unserviceable 201-299, 401-499
 Refer to the MMEL TASK: 413 001-049, 051-099 28-40-06-I)a) 101-149, 151-199
 201-299, 401-499 Check of the Fuel Quantity 417 ALL Indicating System, When an Inner Cell Indication is Unserviceable
 Refer to the MMEL TASK: 417 ALL
 28-CONTENTS Page 30 Aug 01/05 R CES


 CHAPTER 28
__________
 FUEL
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ 28-40-06-I)b) Check of the Fuel Quantity 421 ALL Indicating System, When the Center Tank Indication is Unserviceable
 Refer to the MMEL TASK: 421 ALL
 28-40-06-I)c) Transfer Valve Indication -425 001-049, 051-099 Intercell Transfer 101-149, 151-199
 201-299, 401-499 Refer to the MMEL TASK: 425 001-049, 051-099 28-40-06-E) 101-149, 151-199
 201-299, 401-499 Engine LP Valve Indication - When 430 ALL ECAM Display Inoperative
 Refer to the MMEL TASK: 430 ALL
 28-40-06-B)
 QUANTITY INDICATING 28-42-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 2 ALL System Description 10 ALL Power Supply 12 ALL Interface 14 ALL Component Description 26 ALL FQI Computer (FQIC) 3QT 26 001-049, 051-099 101-149, 151-199 201-299, 401-499 On-Board Replaceable Memory 28 001-049, 051-099 (OBRM) Module (3QT1) 101-149, 151-199 201-299, 401-499 FQI Computer (FQIC) 3QT 28 301-399, On-Board Replaceable Memory 29 301-399, (OBRM) Modules 3QT1 FQIC - ARINC 429 Data Output 30 ALL Fuel Quantity Preselector 5QT 60 ALL Multi-Tank Indicator 6QT 60 ALL FQI Probe 61 001-049, 051-099 101-149, 151-199 201-299, 401-499 FQI Probe 61 301-399, Cadensicon 19QT1(19QT2), 20QT 72 001-049, 051-099 101-149, 151-199 201-299, 401-499 Ultracomp (50QT, 52QT) 73 301-399, Dualcomp (53QT) 73 301-399,
 28-CONTENTS Page 31 Aug 01/05 R CES


 CHAPTER 28
__________
 FUEL
 TABLE OF CONTENTS
_________________
 SUBJECT_______  CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ FQI Probe Shorting Plug 76 001-049, 051-061 Connectors 4041VC-A (4042VC-A) 101-105, 201-203 and 4043VC-A (4044VC-A) 301-399, FQI Probe Fused Plug Connectors 76 001-049, 051-099 4041VC-A (4042VC-A) and 4043VC-A 101-149, 151-199 (4044VC-A) 201-299, 401-499
 Operation/Control and Indicating 77 ALL Operation/Control 77 ALL Refuel/Defuel Operations (Ref. 78 ALL 28-25-00) Accuracy 84 ALL FUEL QUANTITY PROCESSOR -07 87 001-049, 051-099 SOFTWARE 101-149, 151-199
 201-299, 401-499 Input Parameters and BIT 93 001-049, 051-099 Indications 101-149, 151-199
 201-299, 401-499
 Trouble Shooting Data A 0  001-049, 051-099 101-149, 151-199 201-299, 401-499
 Test A 4 ALL Power-up Tests Initialization A 5 001-049, 051-099 and Cockpit Effects 101-149, 151-199
 201-299, 401-499 Power-up Tests Initialization A 15 301-399, and Cockpit Effects
 QUANTITY INDICATING  28-42-00
 DEACTIVATION/REACTIVATION 401 ALL
 CHECK OF THE FUEL QUANTITY 401 ALL
 INDICATING COMPUTER STATUS
 
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