Aircraft Dual Electrical System Trainer

ELC-100D

The Aircraft Dual Electrical System Trainer is a comprehensive system that is ideal for trainings on an aircraft dual-engine electrical system. By using this trainer, students both learn the functionality of each component, and develop logical and systematic approach to perform troubleshooting tasks.

The system is designed to depict a typical aircraft electrical system, and contains standard aircraft components and wiring. Model ELC 100D is a complete functional simulation of a dual-engine 28V DC electrical system include in 115/26 VAC 400 Hz system

Features:

Understanding fundamentals of aircraft Electrical System and its components
Typical aircraft Dual Electrical System
Instructor’s fault panel for introduction (10 simulated faults)
Typical Cockpit Instrumentation, Circuit Breakers, and Controls
Digital Instrument Panel (ECAM) System
Analog Instruments
DC and AC powers
Representative DC and AC Loads
AC and DC bus system (Main, Auxiliary, Bus, Gen, AC, Avionics)
Internal and External Lights
Split bus system
Battery charging system
Distribution terminal strip
Genrators and battery should be in a box under the trainer with transparent plexiglass in front
All components should be connected via terminals.

Components:

Control Panel
- All Bus control switch
- All Load controls
- Nav light control
- Beacon control
- Volt meter selector knob
- External lights control switches
- İnternal lights control switches
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
Relays
- Two ac bus relay
- Two ac bus 26 vac relay
- Generator bus 1 relay
- Generator bus 2 relay
- Battery bus relay
- Main bus relay
- Two Auxiliary- (Non-esential) bus relay
- External power bus Relay
- Avionics bus relay
- Battery relay
- Generator relay
- Blower relay
- Starter relay
- Reverse current relay
Electromechanical Loads Generator
- Landing Gear Motor
- Cabin Air Blower
- Electromechanical Actuator Starter engine
- Two 24-volt starter
External Lights
- Navigation Lights with Strobes
  - Right wing
  - Left wing
  - Tail
- Beacon
- Landing Light
- Taxi Light
Bus bars
- Two ac bus 115 vac 400hz
- Two ac bus 26 vac 400hz
- Two gnd bus
- Generator bus 1
- Generator bus 2
- Battery bus
- Main bus
- Two Auxiliary- (Non-essential) bus
- External power bus
- Avionics bus
Internal Lights
- Cabin Light
- Reading Light
- Multifunction Cockpit Light with Dimmer
Instruments
- Digital Instrument Panel (ECAM)
  - All bus voltmeter
  - All bus status should be illustrated
  - All switch positions
- Load status
- Two Analog Voltmeter
- Analog Ammeter
- Two Hour meter
- Analog Pressure Gauge
- Analog Temperature Gauge
- Two Analog Fuel Level Gauge
Wiring
- Aircraft wires, with clear identification la- bels for each wire.
- All wires are coded and labeled for trouble- shooting.
- Electrical driven by 230 VAC/50 Hz Motor.
Generator Controls (For Two Generator)
- Electronic Controlled Generator
- Driven motor control switch and light
- Driven motor speed control knob
- Voltage regulators
AC Powers
- One Static Inverters 115VAC @ 400 Hz.
- One static inverter 26VAC @ 400 Hz
DC Powers
- Two 28-volt generator driven by electrical motor
Aircraft EPU plug
Aircraft EPU Socket

The system mounted on a metal/aluminum mobile stand.
Metal/aluminum frame with 4 wheels. 2 of 4 wheels are lockable.
Training video for teachers
Delivered fully assembled tested and ready to operate
Colored Ultraviolet printing method on aluminum composite panel

Documentation:

User’s Manual
Study Guide
Instructor’s Guide
Wiring Diagrams
Components Diagrams

Power Specs

Electrical box
Residual current device
Emergency Button
Energy Signal Lamp
110 VAC 60 Hz or 220-240 VAC 50 Hz

Dimensions and weight

Height: Width: Depth: