5 LeftPitotTubeHeatContactorandSolenoid
35 Left Windshield HeatingElements
5 LeftWindshieldHeatingSolenoid
5 FuelQuantityIndicatingSystem
5 WingandTailDeiceEngageValve
WingandTailDeiceIndicator
WingandTailDeiceTimer
5 CockpitLeftPanelLights
5 CockpitCenterPanelLights
5 CockpitRightPanelLights
15 LogoLights
10 LandingLights
10 TaxiLight
5 LeftWing(Red),RightWing(Green),and
TailBullet(White)Lights
10 Left and RightWingStrobeLights
5 GearLockedDownIndicatorLights
GearNotLockedWarningLight
GearDoorSwitch
5 GearSelectorSolenoidLock
GearDoorSolenoid
GearWarningHorn
GearWarningMuteSwitch
15 Number1 dc to ac PowerInverter
3 ElectricTrim Servo Power
2 Pilot'sAudioSelectorBoxPower
3 Pilot's Altimeter servoPower
5 AnnunciatorMalfunctionWarningLight
5 AnnunciatorMasterWarningand Test Circuit
5 LeftStarterGeneratorReset
5 RightStarterGeneratorReset
10 LeftStarterGeneratorVoltageControl
10 RightStarterGeneratorVoltageControl
5 LeftSideLeftComputerPower
15 Left Side LeftTransducerHeat
EFFECTIVITY:
A: 040, 045-050
B: 040-999 Jan 10/90 9
24-60-00 PAGE
PIPER AIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCE MANUAL
A. DC Electrical Load Distribution (continued)
CHART 4 BREAKERFUNCTION-LEFT BREAKER PANEL (Sheet 3 of 3)
USED ON CODE CIRCUIT BREAKER BREAKER VALUE(AMPS) CIRCUIT PROTECTED
C WINGINSPECTION
C RECOG LIGHTS
C q-SENSOR
C FLUORESCENTLIGHTS
GLARESHIELD
C FLUORESCENTLIGHTS
BRIT/DIM
C VG1
C RADAR
C VG2
A GPWS
A VOICE RECORD
C AIR SPD 1
C EHSI HDG
C EADI ATTD
C AP
C NAV1
C COMP 1
C RMI 1
A UNS1
B FCS
5 Wing Inspection Light
10 Left and Right Recognition Lights
3 DynamicPressureSensor Switch
5 Pilot's and Copilot's FluorescentFlood Lights
Pilot's and Copilot's Fluorescent
5 Flood Lights Intensity
1 Pilot's Attitude Gyro and Flight Director
1 Radar Antenna
1 Copilot'sAttitudeGyro and Flight Director
2 Ground Proximity Warning System
1 FairchildCockpit Voice Recorder Unit
1 Number1 Airspeed Indicator
1 HorizontalSituationIndicator Heading Flag
Number1 Multifunction PRocessingUnit
Number1 Display Processing Unit
1 ElectronicAttitude Display Unit Flag
Number 1 Multifunction ProcessingUnit
Number 1 Display Processing Unit
1 AutopilotComputer,Yaw Rate Gyro
1 Number 1 Very High Frequency
NavigationReceiverac Power
1 Number1 Compass System
1 Number 1 Radio Magnetic Indicator
Number1 VOR on RMI 1
1 UniversalNavigationSystem
1 Flight Control System Power
MultifunctionProcessingUnit
Display Processing Unit
EFFECTIVITY:
A: 048-050
B: 040-047
Jan10/9024-60-00
C: 040-999
PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
A. DC Electrical Load Distribution (continued)
CHART 5 BREAKERFUNCTION-RIGHTBREAKERPANEL (Sheet 1 of 4)
USED CIRCUIT BREAKER CIRCUIT
ON CODE BREAKER VALUE(AMPS) PROTECTED
BLEEDAIR CONT 3 RightEngineBleedAir Valve
TORQUEMETER 3 RightEngineTorqueIndicatingSystem
OILCOOLER 5 RightEngineOil Cooler Door
OILTEMP 3 RightEngineOil TemperatureIndicatingSystem
OIL PRESS 3 RightEngineOil PressureIndicatingSystem
FUELPRESS 5 RightEngineFuel PressureIndicatingSystem
FUELFLOW 5 RightEngineFuelFlowIndicatingSystem
OXYGENCONTROL 3 EmergencyOxygenMaskDeploymentSolenoid
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：夏延飞机维护手册 Cheyenne IIIA PA-42-720 AMM 1(85)
