Aircraft Hydraulic Landing Gear System Trainer (Advance) V.2


HYD-100V 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. It contains all components and assemblies of an actual hydraulic landing gear system.
Model HYD – 100V features complete wheel and tire assembly with hydraulic brake system, including master cylinder and brake pedal. The control unit includes control throttles for landing gear and hydraulic flap operation. Indicators demonstrate show up, down, and in-transition conditions. A throttle warning horn is also mounted on the control panel.
This model comes mounted on a mobile stand to provide a clear view from all directions.


  1. Understanding fundamentals of aircraft hydraulic landing gear system and its components.
  2. Some of Trainer Functions
    • Landing gear extension functions
    • Landing gear retraction functions
    • Gravity lever functions
    • Speed brake lever functions
    • Flap lever functions
    • Brake functions
    • Park brake functions
    • Hydraulic power functions
    • Accumulator functions
    • Emer hand pump functions
    • Pumps fault functions
    • ECAM functions
    • Single chime functions
    • Master caution functions
    • Master warning functions
    • Check valves functions
  3. Some of Trainer Processes
    • Landing gear extension test process
    • Landing gear retraction test process
    • Aircraft jacking process
    • Hydraulic system functional test process
    • Hydraulic system leak test process
    • Hand pump test process
    • Accumulator test process
    • ECAM test process
    • Emergency system test process
  4. Some of Trainer Cases
    • Low level
    • Over heat
    • Low air pressure
    • Engine fire
    • System Leak
    • Fuel pump fault
  5. Hydraulic Flap System
  6. Brake System
  7. Aircraft Wheel System
  8. Hydraulic System Control
  9. Lower ECAM (on the main unit)
  10. Master Caution System
  11. Aural warning Horn Panel System
  12. Hydraulic Landing Gear Trainer able to display the landing gear operating system of a regular aircraft.
  13. Digital sensor data and switch states used in the set.
  14. Throttle lever with associated components complete the warning circuit of gear up warning horn.
  15. the accumulator and the hand pump be able to control the landing gear.
  16. Wirings on the trainer are connected via terminals.
  17. Wires should have clear identification labels for each wire.
  18. All wires should be coded and labeled for troubleshooting.
  19. Instructor’s panel for Fault Insertion


  1. Electrically Driven Hydraulic Pump
  2. Hydraulics Filter
  3. Flap/Aileron control solenoid
  4. Emergency Hand Pump
  5. Hydraulic Fluid Reservoir
  6. Hydraulic Accumulator with automatic filling system
  7. Hydraulic System analog pressure gauge
  8. Valve pressure sender
  9. Hydraulic System Pressure sender
  10. Hydraulically Operated Landing Gear Mechanism
  11. Drain Valve
  12. Hydraulic Actuating Cylinder for Landing gear
  13. Hydraulic Actuating Cylinder for Landing gear door
  14. Check valve
  15. Hydraulic System analog pressure gauge
  16. Hydraulic System Pressure sender
  17. Brake pressure gauge
  18. Hydraulic Sequencing System and operate
  19. Hydraulic Flap System
  20. Hydraulic flap Actuating
  21. Flap Position Sensors
  22. Flap control switch
  23. Cutaway or Mock-up Flap
  24. Aircraft Tire Assembly (6 or 8 inch)
  25. Aircraft Tire
  26. Aircraft Wheel
  27. Aircraft Brake disk
  28. Aircraft Brake Plate
  29. Aircraft Brake caliber
  30. Hydraulic Brake Components
  31. Aircraft Brake master cylinder
  32. Park brake
  33. Brake Fluid Reservoir
  34. Aircraft Brake Pedal
  35. Brake Hose
  36. Throttle Lever (TQ)
  37. Control Panel
    • Circuit brakers
    • Aircraft Circuit breaker lockout
    • Lockable Landing gear control lever
    • Power Panel
    • Aircraft Landing gear control panel
    • Landing gear status lamp
    • Lockable Flap control panel/lever (pullable)
    • Lockable speed brake control panel/lever (push able)
    • Landing Gear door control lamp
    • Energy Lamp
  38. Lower EICAS or ECAM (10 inch on the main unit)
    • Landing gear position
    • Landing door position
    • Pressure gauge
    • Sensor’s status
    • Landing gear system control
    • Throttle Lever Position
    • Speed brake position
  39. Other
    • Ten (10) cotters for aircraft tire
    • One (1) Analog tire pressure gauge for aircraft tire
  • 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


  • User’s Manual
  • Study Guide
  • Instructor’s Guide
  • Flow 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: 170cm Width: 135cm Depth: 165cm
  • Weight: 230kg