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AVIATION 325 ELECTRICAL SYSTEM
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Electrical System General Description Sources of Electrical Power
Power Distribution Normal Conditions Abnormal Conditions
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General Description 14 Volt Dual Fed Split Bus Negative Ground
DC System
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Sources of Electrical Power
Battery External Power Unit Alternators
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Battery 12 Volt, 35 Amp-Hr Lead Acid Drains & Vents Recharge
Battery Bus Battery Master Switch Battery Contactor Starter Contactors Tie Bus (60 Amps)
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External Power Receptacle
Location Energizes External Power Contactor Starter Contactors Tie Bus Prior to Energizing Battery Master Off All Electrical Equipment Off
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Alternators 14 Volts AC, 70 Amp Rectifier (AC to DC) Belt Driven
Alternator Field Main Bus 5 Amps Alternator Switch Location
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Alternators Alternator Control Unit Voltage Regulator
Over Voltage Relay Load Sharing
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Alternators An overvoltage relay if output exceeds 17 volts.
Voltage regulator maintains effective load sharing. Location
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System Monitors ALT Annunciator Light - ALT Switch Turned Off
Over Voltage Relay Low Bus Annunciator less than 17.5 volts Ammeter Load Meter Circuit Breakers
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Power Distribution Battery Bus Tie Bus Main Bus Non-Essential Bus
Avionics Bus
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Battery Bus Hot Wired Fuses Equipment Clock Flight Time Hour Meter
Maintenance Time Hour Meter Heater Hour Meter
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Power Distribution Tie Bus Main Bus Non Essential Bus
Essential Electrical Components Tie Bus - Two 60 Amp Circuit Breakers Non Essential Bus
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Power Distribution Avionics Bus #1 Avionics Bus #2 Radio Master
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Circuit Breaker Panel
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Circuit Breaker Panel
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Abnormal Conditions Alternator Failure Circuit Breaker Over Voltage
Mechanical Failure ALT Light
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Abnormal Conditions Single Alternator Failure Alt Annunciator Light
Ammeter Reduce Load Dual Alternator Failure Alt Annunciator Lo Bus Battery Load Shedding
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Electrical Failure Scenario
Okay,you loose your alternators, and you are flying on battery power alone. You’ve just departed on an IFR flight , but the weather is still VFR – you haven’t hit IMC yet. What do you do? Turn back right?
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Quiz The over voltage relay will take its respective alternator offline if . . . A. the electrical system’s voltage exceeds 17 volts. B. the alternator’s output voltage exceeds 17 volts.
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