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时间:2011-03-25 17:44来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 Indicating and Warning 1 ALL Component Location 1 ALL System Description 4 ALL Power Supply 4 ALL Interface 4 ALL Component Description 4 ALL Operation/Control and Indicating 4 ALL BITE Test 4 ALL
 POSITION AND WARNING 32-60-00
_____________________
 ADJUSTMENT/TEST 501 ALL Anti Skid Indication on ECAM WHEEL 501 ALL Page
 Refer to the MMEL TASK: 501 ALL 32-60-03-F)
 INDICATING AND WARNING 32-61-00
 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL System Description 1 ALL Position Data 5 ALL Indication 5 ALL Cautions and Warnings 6 ALL L/G Control Lever 6 ALL Power Supply 6 ALL Interface 6 ALL LGCIU - ARINC 429 Output Data 6 ALL Component Description 23 ALL
 32-CONTENTS Page 55 Aug 01/05
 CES

 

 CHAPTER 32
__________
 LANDING GEAR
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Cockpit Panel 23 001-049, 051-099 101-149, 151-199 201-299, 301-399 Cockpit Panel 30 401-499, L/G Control-Lever (6GA) 34 ALL Operation/Control and Indicating 34 ALL Normal System Indications 34 ALL L/G System Warnings 35 ALL WHEEL Page - Single System 43 ALL Failure Indications L/G Free-Fall Extension 44 ALL
 BITE Test 44 ALL
 INDICATING AND WARNING 32-61-00
 DEACTIVATION/REACTIVATION 401 ALL
 Operational Check of the ECAM 401 ALL
 Landing Gear NOT DOWN Warning

 Refer to the MMEL TASK: 32-60-02 401 ALL
 INDICATING AND WARNING 32-61-00
 ADJUSTMENT/TEST 501 ALL
 BITE Check Using MCDU to Ensure 501 ALL
 "Gear NOT DOWN for Landing"
 Warnings Operative

 LANDING GEAR - POSITION INFORMATION 32-62-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL System Description 1 ALL Power Supply 4 ALL Interface 4 ALL
 LANDING GEAR - BITE 32-69-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL System Description 1 ALL Failure Monitoring 1 ALL BITE Test 3 ALL Failure Data 3 ALL Landing Gear Simulation Function 5 ALL CFDS 5 ALL Power Supply 11 ALL
 32-CONTENTS Page 56 Aug 01/05
 CES

 

 CHAPTER 32
__________
 LANDING GEAR
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Interface 11 ALL Component Description 11 ALL Operation/Control and Indicating 11 ALL Failure Conditions 19 ALL BITE Test 33 ALL
 LANDING GEAR - BITE 32-69-00
 ADJUSTMENT/TEST 501 ALL BITE Test of the Landing Gear 501 ALL Simulation of Flight, with the 505 ALL Aircraft on the Ground
 32-CONTENTS Page 57 Aug 01/05
 CES


 LANDING GEAR - GENERAL - DESCRIPTION AND OPERATION
__________________________________________________
R
 1. Glossary
________
 -------------------------------------------------------------------------------| ABBREVATION | SIGNIFICATION | -------------------------------------------------------------------------------| ACARS | Arinc Communications Addressing and | | | Reporting System | | ACSC | Avionic Compartment System Cooling | | ADIRU | Air Data Inertial Reference Unit | | ADF | Automatic Direction Finding | | AEVC | Avionics Equipment Ventilation Controller | | AIDS | Aircraft Integrated Data System | R | APU | Auxiliary Power Unit | | ARINC | Aeronautical Radio Incorporated | | ATC | Air Traffic Control | | BITE | Built-In Test Equipment | | BRK | Brake | | BSCU | Brakes and Steering Control Unit | | C/B | Circuit Breaker | | CFDIU | Centralized Fault Display Interface Unit | | CFDS | Centralized Fault Display System | | CIDS | Cabin Intercommunication Data System | | CMPTR | Computer | | CONFIG | Configuration | | CRT | Cathode Ray Tube | | DFDR | Digital Flight Data Recorder | | DMC | Data Management Computer | | DME | Distance Measuring Equipment | | DU | Display Unit | | EFCS | Electronic Flight Control System | | EIS | Electronic Instrumentation System | | FAC | Flight Augmentation Computor | | FADEC | Full Authority Digital Engine Control | | FCDC | Flight Control Data Concentrator | | FGC | Flight Guidance Computer | | FIN | Functional Item Number | | FWC | Flight Warning Computer | | GPWS | Ground Proximity Warning System | | HF | High Frequency | | HP | High Pressure | | ILS | Instrument Landing System | | KT | Knot(s) | | LG | Landing Gear |

 1EFF : ALL  1 32-00-00Page 1
 1 1 May 01/03 1 1 1CES 1 -------------------------------------------------------------------------------| ABBREVATION | SIGNIFICATION | -------------------------------------------------------------------------------| LGCIU | Landing Gear Control and Interface Unit | | LH | Left Hand | | LP | Low Pressure | | LRU | Line Replaceable Unit | | MLG | Main Landing Gear | | MRDS | Maintenance and Recording Data System | | NLG | Nose Landing Gear | | N/W | Nose Wheel | | PSI | Pounds per Square Inch | | RAM | Random Access Memory | | RH | Right Hand | | RMP | Radio Management Panel | | ROM | Read Only Memory | | SDAC | System Data Aquisition Concentrator | | SDI | Source Data Identifier | | STG | Steering | | TPIS | Tire Pressure Indicating System | | VHF | Very High Frequency | | VLE | Maximum Landing Gear Extended Speed | | VLO | Maximum Landing Gear Operating Speed | | VOR | Very High Frequency Omniidirectional Range | -------------------------------------------------------------------------------
 
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