Features:

1. Understanding fundamentals of aircraft Electrical System and its components
2. Typical aircraft Single Electrical System system.
3. Typical Cockpit Instrumentation, Circuit Breakers, and Controls
4. Digital Instrument Panel (ECAM) System
5. Analog Instruments
6. DC and AC powers
7. Representative DC and AC Loads
8. AC and DC bus system (Main, Auxiliary, Bus, Gen, AC, Avionics)
9. Internal and External Lights
10. Battery charging system
11. Distribution terminal strip
12. Battery are in a box under the trainer with transparent plexiglass in front
13. All components connected via terminals.

Components:

1. Control Panel
   • All Bus control sw
   • All Load control
   • Nav light control
   • Beacon control
   • Volt meter selector knob
   • External lights control switches
   • Internal lights control switches
2. Breaker (CB) Panel
   • Generator CB
   • NAV CB
   • Avionic CB
   • Beacon CB
   • Actuator CB
   • Main Bus CB
   • Blower CB
   • Auxiliary- (Non- essential) CB
   • External power bus CB
   • Circuit breaker lockout
3. Relays
   • One ac bus relay
   • One ac bus 26 vac relay
   • Generator bus 1 relay
   • Battery bus relay
   • Main bus relay
   • One Auxiliary- (Non- essential) (bus relay)
   • External power bus Relay
   • Battery relay
   • Generator relay
   • Blower relay
   • Starter relay
4. Electromechanical Loads Generator
   • Landing Gear Motor
   • Cabin Air Blower
   • Electromechanical Actuator Starter engine
   • One 24 volt starter
5. External Lights
   • Navigation Lights with Strobes
   • Right wing
   • Left wing
   • Tail
   • Beacon
   • Landing Light
6. Bus bars
   • One ac bus 115 vac 400 Hz.
   • One ac bus 26 vac 400 Hz.
   • One GND bus
   • Generator bus 1
   • Battery bus
   • Main bus
   • One Auxiliary- (Non- essential) bus
   • External power bus
   • Avionics bus
7. Internal Lights
   • Cabin Light
   • Reading Light
   • Multifunction Cockpit Light
8. Instruments
   • Digital Instrument Panel (ECAM)
     • All bus voltmeter
     • All bus status illustrated
     • All switch positions
   • Load status
   • One Analog Voltmeter
   • Analog Ammeter
   • One Hour-meter
   • Analog Pressure Gauge
   • Analog Temperature Gauge
   • One Analog Fuel level Gauge
9. Wiring
   • Aircraft wires, with clear identification labels for each wire.
   • All wires are coded and labeled for trouble- shooting.
   • Electrical driven by 230 VAC/50 Hz Motor.
10. Generator Controls (for two generator)
    • Electronic Controlled Generator
    • Driven motor control switch and light
    • Driven motor speed control knob
11. AC Powers
    • One Static inverters 115VAC @ 400 Hz.
    • One static inverter 26VAC @ 400 Hz
12. DC Powers
    • One 28 volt generator driven by electrical motor
13. Aircraft EPU plug
14. Aircraft EPU Socket