Aircraft Electrical Landing Gear Trainer

HYD-100E

HYD-100E Landing Gear Module for offers effective hands-on training for aircraft landing gear system maintenance trainees. It assures that technicians are trained to maintain the landing gear system in the best way possible and in accordance with safety standards. It displays the landing gear mechanism as found in actual aircraft. This trainer is designed to represent a landing gear system.

Features:

  1. Electrical Landing Gear Trainer able to display the landing gear operating system of a regular aircraft.

  2. Landing gear actuator controlled via electric driven motor.

  3. Digital sensor data and switch states used in the set.

  4. Wirings on the trainer are connected via terminals

  5. Wires have clear identification labels for each wire

  6. All wires are coded and labeled for troubleshooting

  7. The system mounted on a metal/aluminum mobile stand

  8. Metal/aluminum frame with 4 wheels. 2 of 4 wheels are lockable

  9. Delivered fully assembled tested and ready to operate

  10. Colored Ultraviolet printing method on aluminum composite pane

Components:

  1. Control Panel
    • Landing Gear Down and Lock Lights
    • Landing Gear Transition Light

    • Lockable Landing Gear Lever

    • Master Caution System

    • Aural Warning Horn

    • Circuit breaker

    • Aircraft Circuit breaker lockout

    • Test Button

  2. Throttle lever with associated components complete the warning

  3. Landing gear electric motor

  4. Landing gear actuator

  5. Aircraft wheel system

  6. Aircraft Tire Assembly (6 or 8 inch)

    • Aircraft Tire

    • Aircraft Wheel

Documentation:

  • Operations Manual
  • Training video for Instructors

Power Specs

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

Upgrades

  • HYD-100E-WNG Wing cross section that contains electrically operated flap and spoiler surfaces upgrade

  • HYD-100E-ASMD Aircraft Systems Monitoring Display that represents the ECAM/EICAS system in aircraft. It is used to check the landing gear position upgrade.