Presentation is loading. Please wait.

Presentation is loading. Please wait.

AVIATION 325 ELECTRICAL SYSTEM.

Similar presentations


Presentation on theme: "AVIATION 325 ELECTRICAL SYSTEM."— Presentation transcript:

1 AVIATION 325 ELECTRICAL SYSTEM

2 Electrical System General Description Sources of Electrical Power
Power Distribution Normal Conditions Abnormal Conditions

3 General Description 14 Volt Dual Fed Split Bus Negative Ground
DC System

4 Sources of Electrical Power
Battery External Power Unit Alternators

5 Battery 12 Volt, 35 Amp-Hr Lead Acid Drains & Vents Recharge
Battery Bus Battery Master Switch Battery Contactor Starter Contactors Tie Bus (60 Amps)

6 External Power Receptacle
Location Energizes External Power Contactor Starter Contactors Tie Bus Prior to Energizing Battery Master Off All Electrical Equipment Off

7 Alternators 14 Volts AC, 70 Amp Rectifier (AC to DC) Belt Driven
Alternator Field Main Bus 5 Amps Alternator Switch Location

8 Alternators Alternator Control Unit Voltage Regulator
Over Voltage Relay Load Sharing

9 Alternators An overvoltage relay if output exceeds 17 volts.
Voltage regulator maintains effective load sharing. Location

10 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

11 Power Distribution Battery Bus Tie Bus Main Bus Non-Essential Bus
Avionics Bus

12 Battery Bus Hot Wired Fuses Equipment Clock Flight Time Hour Meter
Maintenance Time Hour Meter Heater Hour Meter

13 Power Distribution Tie Bus Main Bus Non Essential Bus
Essential Electrical Components Tie Bus - Two 60 Amp Circuit Breakers Non Essential Bus

14 Power Distribution Avionics Bus #1 Avionics Bus #2 Radio Master

15 Circuit Breaker Panel

16 Circuit Breaker Panel

17 Abnormal Conditions Alternator Failure Circuit Breaker Over Voltage
Mechanical Failure ALT Light

18 Abnormal Conditions Single Alternator Failure Alt Annunciator Light
Ammeter Reduce Load Dual Alternator Failure Alt Annunciator Lo Bus Battery Load Shedding

19 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?

20 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.

21 end


Download ppt "AVIATION 325 ELECTRICAL SYSTEM."

Similar presentations


Ads by Google