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Hydraulic System Main Unit (Module)

UHT-100V

Aircraft Hydraulic System Trainer provides students with practical experience needed to understand the function, to get to know components and to improve troubleshooting skills. Fully functional hydraulic system designed so that every component can be disassembled, reassembled and functionally tested. All the components mounted on the trainer are operational, removable and they can be reinstalled.

NOTE: EICAS/ECAM screen is located on the hydraulic landing gear trainer or main unit.

NOTE: Hydraulic System Main Unit UHT-100V is basically a hydraulic power unit which provides hydraulic pressure to operate the HYD-100V Landing Gear Module. UHT-100V can not be operated without HYD-100V

Features:

  1. Understanding fundamentals of aircraft hydraulic system and its components.
  2. Hydraulic control solenoids
    • Flap
    • Speed Brake
    • Landing Gear
    • Landing Gear Door
  3. System is powered by Hydraulics Pump, Hand Pump or Accumulator
  4. Some of Trainer 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
  5. Some of Trainer Processes
    • Hydraulic system functional test process
    • Hydraulic system leak test process
    • Emergency system test process
    • Automatic accumlator filling process
  6. All wires should be coded and labeled for troubleshooting.
  7. The hardware used in the trainer is mounted to the frame in a way that it can be easily observable by students.
  8. The system mounted on a metal/aluminum mobile stand.
  9. Metal/aluminum frame with 4 wheels. 2 of 4 wheels are lockable.
  10. Delivered fully assembled tested and ready to operate
  11. Colored Ultraviolet printing method on aluminum composite panel

Components:

  1. Control Panel
    • Press to test illuminated Master warning button
    • Press to test illuminated Master caution button
    • Aural warning horn
    • Fire warn indicator
    • Hydraulic pump control illuminated pushbutton
    • Leak measurement valve control illuminated pushbutton
    • Hydraulic pump fault indicator
    • Three (3) units Aircraft circuit breaker
    • Guarded master power SW
  2. 10-inch touchable screen ECAM
    • Landing gear position (real time)
      • Up locked
      • Transit
      • Down locked
    • Landing door position
    • HYD tank status
      • Temp Sensor
      • Pressure Sensor
      • Level Sensor
    • Pressure gauge
    • Flap position
    • Speed brake position
  3. Aircraft circuit breaker lockout
  4. Electrically Driven Hydraulic Pump
  5. Hydraulic Fluid Reservoir
  6. Hydraulics Filter
  7. Landing gear control solenoid
  8. Landing gear door control solenoid
  9. Flap control solenoid
  10. Speed Brake control solenoid
  11. Emergency Hand Pump
  12. Hydraulic Accumulator with automatic filling
  13. Hydraulic System analog pressure gauge (8 pieces)
  14. Sensors
    • Tank temperature sensor
    • Tank level sensor
    • Hydraulic System Pressure sensor
  15. Drain Valve
  16. Check valve
  17. LAN output
  18. Terminals

Documentation:

  • User’s Manual
  • Study Guide
  • Instructor’s Guide
  • Training video for teachers

Power Specs

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

Required Items

  • Aircraft Landing Gear System Trainer HYD-100V
  • DTE-10 Hydraulic Oil 5 Liters
  • DTE-46 Hydraulic Oil 28 Liters

Accessories

  • Instructor’s Panel Control Application (without computer) for Scenario and
    Fault Simulation