Aircraft Turbine Fuel System Trainer (2 Tanks)

FCU-100B

Designed to represent a complete aircraft fuel system, Model FCU – 100B Turbine Fuel System Training Set enables trainees to learn the essentials of fuel system components and how these components are linked to each other in a typical aircraft fuel system.

This trainer includes a capacitance fuel system that shows non-linear fuel quantity indications with multiple probes set at various angles. It comes fully plumbed and with a wing tank.

This completely functional fuel system consists of a fuel management panel, fuel transfer system and capacitance fuel quantity indicating system. It also contains an instructor’s panel that makes it possible to add faults to conduct troubleshooting training.

The fuel system panel features fuel quantity indicators, a fuel transfer selector valve, fuel transfer and low fuel warning lights, fuel pressure and flow indicators and complete fuel system drawings.

This system contains, engine driven fuel pump screen, fuel filter, fuel control unit, turbine fuel nozzle inside a clear enclosed container etc.

Features:

  1. Understand fundamentals of aircraft fuel system and its components.
  2. Fully functional and configured like a typical aircraft fuel system.
  3. Aircraft fuel system can run automatically and manually.
  4. Fuel tanks are automatically filled and when tank is full system is automatically be shut off.
  5. The control of the fuel that flows to combustion chamber can be observed using the throttle lever.
  6. Fuel tanks have a maintenance hatch.
  7. Fuel tanks be manually drained for maintenance.
  8. Fuel tanks have transparent window in order to observe fuel filling and refilling.
  9. Combustion chamber is transparent.
  10. Tanks are able to manually or automatically cross-fit.
  11. Aircraft fire scenario is simulated.
  12. The hose and tubes used in the trainer are labeled according to aviation
  13. Wirings on the trainer are connected via terminals.
  14. Wires have clear identification labels for each wire.
  15. All wires are coded and labeled for troubleshooting.
  16. All required hoses and pipes
  17. Instructor’s panel for Fault Insertion (Independent Unit)

Components:

  1. Fuel Control Unit (FCU)
  2. Three (3) pieces minimum mock-up fuel tank
  3. A minimum 40 Lbs. aircraft refuel tank
  4. Three (3) pieces fuel pump
  5. Three (3) Level control switches
  6. A refuel pump
  7. Engine no:1 Combustion chamber
  8. Fuel Nozzle
  9. Throttle lever
  10. Fuel filter
  11. Cross feed control valve
  12. Fuel Pressure sender
  13. Fuel Level Sender
  14. Fuel Flow Sensor
  15. Shut-Off Valve
  16. Control panel
  17. 10” inch touchable screen
  18. Terminals
  19. Three (3) manuals drain valve
  20. Check valves
  21. LAN output
  22. Control Panel
  23. Master power panel
  24. Master caution panel
  25. Aural warning horn
  26. Left pump control switch
  27. Right pump control switch
  28. Main pump control switch
  29. Test button
  30. Status lamps
  31. Aircraft circuit breaker
  32. Aircraft circuit breaker lockout
  33. Pressure relief bypass valve
  34. 10” inch touchable screen (like EICAS or ECAM)
    • Left tank fuel quantity indicator
    • Right tank fuel quantity indicator
    • Fuel pressure indicator
    • Fuel flow indicator
    • Switch Position
    • Valve status
  • 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
  • Components Diagrams
  • Flow 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: