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时间:2011-04-25 08:35来源:蓝天飞行翻译 作者:航空
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

EMERGGEAREXT  7.5  EmergencyLandingGear Extension(NOTE: 
7 and 7.5 amp breakersareratedequally) 
FUELPUMP  10  RightEngineElectricFuelPump 
STALLCONT  5  RightSideLiftComputerPower 
STALLHEAT  15  RightSideLiftTransducerHeat 
ITT  3  RightEngineInterturbineTemperatureSystem 
STARTCONT  5  RightEngineStartContactor 
IGNITION  5  RightEngineIgnitor 
RightEngineIgnitionMonitorRelay 
RightEngineAutomaticIgnition 
TorqueSwitch 
HTGRESET  5  RightEngineHydraulicToppingGenerator 
ResetSwitchand Solenoid 
ICE VANE ANDCONT  7.5  RightEngineIceDeflectorDoorMotor,Relays, 
and Indicator. 
AIR INTAKE DEICE  30  RightEngineAir IntakePartingStrip 
RightEngineShedArea I 
RightEngineShedArea II 
PROPDEICE  30  RightPropellerLip Deicerand DeicerTimer 
RightPropellerInboardHeatingElements 
RightPropellerOutboardHeatingElements 
WINDSHIELDWIPER  10  WindshieldWiperMotor 
R.WINDSHIELDHEAT  35  RightWindshieldHeatingElements 
R. WINDSHIELD CONT  5  RightWindshieldHeatSolenoid 
R. PITOT HEAT  5  RightPitotTubeHeatElementand Contactor 
HOURMETER  3  HourMeterInstrument 

EFFECTIVITY: 
040-999P24-60-00  AGE11 
24-60-00  Jan 10/90 

PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL

A. DC Electrical Load Distribution (continued)
CHART 5 BREAKER FUNCTION -RIGHT BREAKER PANEL (Sheet 2 of 4)
USED  CIRCUIT 
ON CODE  BREAKER 
A  CABIN COMFORT 
A  RECIR FAN 
A  ECS 
A  READINGLIGHTS 
A  CABINLIGHTS 
A  FLAP MOTOR 
A  FLAP CONTROL 
A  PROP SYNC 
A  AUTO FEATHER 
A  COMMODE PUMP 
A  BEVUNIT 
B  FUEL TOTALIZER 
C  FUEL REMAINING 
TOTALIZER 
A  AUDIO AMP 2 
A  AUDIO 2 
A  COMM1 
A  COMP1 
A  XPNDER 1 
D  EMER GYRO 
A  NAV1 
D  UHF COMM 
A  DME1 

BREAKER  CIRCUIT 
VALUE (AMPS)  PROTECTED 
5  Cabin Temperature Controller 
Cabin Temperature Thermostat 
Hot Air Bypass Valve Switch 
15  RecirculatingFan Motors 
5  Cabin Overtemperature ThermalSwitch 
Cabin Overpressure Switch 
RecirculatingDoor Solenoids 
5  OverheadReadingand Console Lights 
5  Left and Right Cabin Aisle Lights 
35  Flap Motor, Down Solenoid, Up Solenoid 
3  PositionIndicator 
PositionControl Rheostat 
DifferentialControl Rheostat 
Test Switch 
3  PropellerSynchrophaserSystem 
5  AutomaticPropellerFeatheringSystem 
7  CommodePumpPower 
10  BeverageUnit and Razor Inverter 
5  Fuel Totalizer 
5  FuelRemainingTotalizer 
2  Copilot'sAudio Panel and Audio Panel Lighting 
2  ObserverAudioPanel 
7.5  Number1 Very High Frequency 
CommunicationsRadio Power 
3  Number1 Compass System 
2  Pilot's Radar Transponder Power 
5  Pilot and Copilot EmergencyGyro 
2  Number 1 Very High Frequency 
NavigationReceiverdcPower 
5  Ultra High Frequency Communications 
Transmitter/ReceiverPower 
3  Pilot"s Distance MeasuringEquipment 
Radio dc Power 
EFFECTIVITY: 
A: 040-999 

B: 045-047

PAGE12
Jan10/9024-60-00
D: 048-050

PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL

A. DCElectricalLoadDistribution(continued)
CHART 5 
BREAKERFUNCTION-RIGHTBREAKERPANEL (Sheet3 of 4) 
USED  CIRCUIT  BREAKER  CIRCUIT 
ON CODE  BREAKER  VALUE(AMPS)  PROTECTED 
A  EADI1  5  Pilot'sHorizontalSituationIndicator 
A  DCP1  1  Pilot'sDisplayControlPanelPower 
A  DPU1  7.5  Pilot'sDisplayProcessingUnit Power 
A  MPU1  7.5  Pilot'sMultifunctionProcessingUnit Power 
A  MFD  5  MultifunctionDisplayand DisplayFan Power 
 
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本文链接地址:夏延飞机维护手册 Cheyenne IIIA PA-42-720 AMM 1(86)