Autopilot / Automatic Flight Controls Trainer

Order Code: AP-100C

Category: Avionics & Instrument Systems

Autopilot Trainer is an excellent resource for teaching the principles of automatic flight controls by demonstration using a complete system that encompasses all the aspects of three(3) axis autopilot and automatic flight controls. Diffe...



SPECIFICATION

Autopilot Trainer is an excellent resource for teaching the principles of automatic flight controls by demonstration using a complete system that encompasses all the aspects of three(3) axis autopilot and automatic flight controls.

Differences from AP-100B Model

  • Automatic/Motorized Yoke System
  • Automatic/Motorized Rudder Pedal System
  • Automatic/Motorized Throttle Lever
  • Pitch Trim Servo System
  • Heading Feed Back
  • Altitude Feed Back
  • Active Remote Gyro HSI System
  • Flux Detector(The Magnetic Azimuth Transmitter)
  • Slaving Accessory
  • Remote Control Panel
  • Vacuum Pump

 

Specifications
Features

  • Indicators operate in sync with auto-pilot system
  • Aircraft position controlled by yoke.
  • Automatic/Motorized Yoke System
    • Yoke automatically/motorized moves in two axis with data from autopilot computer. It performs automatic positioning according to the position of the airplane.
  • Automatic/Motorized Rudder Pedal System
    • Rudder Pedal automatically/motorized moves in one axis with data from autopilot computer. It performs automatic positioning according to the position of the airplane.
  • Automatic/Motorized Throttle Lever
  • Yoke and rudder pedal can move the control surfaces of the aircraft.
  • Servos operate in sync with auto-pilot and yoke/rudder pedal.
  • 2 axis DOF + 1 DOF system
  • Pitch Trim Servo System
  • Heading Feed Back
  • Altitude Feed Back
  • Active Remote Gyro HSI System
  • Remote Control Panel
  • Vacuum Pump
  • Remote Altitude control & feedback
  • Remote Heading control & feedback
  • Remote side wing control
  • Remote head wing control
  • The aircraft automatically calibrated to runway position when the trainer is turned on.
  • Instructor’s panel for Fault Insertion
  • The system mounted on a metal/aluminum mobile stand.
  • Metal/aluminum frame with 4 wheels. 2 of 4 wheels are lockable.

Components

15-inch PFD-MFD screen
• Attitude Directional Indicator(ADI)
• Directional Gyro(HSI)
• Airspeed Indicator(ASI)
• Altimeter(ALT)
• Vertical Speed Indicator(VSI)
• Turn and Slip Indicator
• Course deviation bar(CDI)
• Course Pointer
• RPM indicator
• Manifold Pressure indicator
• Engine instruments(Oil, Fuel system)

  • Yoke ( Automatic/Motorized )
  • Rudder Pedal ( Automatic/Motorized )
  • Throttle Control ( Automatic/Motorized )
  • Pitch / Yaw / Roll / Pitch Trim servos
  • The trainer should have auto-pilot panel.
    • Active AP(auto-pilot) function button,
    • Active Pitch function button,
    • Active Roll function button,
    • Active ALT(altitude) function button,
    • Active V/S(vertical speed)function button,
    • Active FLC function button,
    • Active HDG(heading) function button,
    • Active FEET function Knob,
    • Active FPM function Knob,
    • Active HDG function Knob,
    • All function buttons should be illuminated.
  • Master Power and Switch panel.
    • DC master power switch,
    • Master power lamp,
    • Beacon switch,
    • Engine Start,
    • PFD circuit breaker,
    • Auto-Pilot circuit breaker,
    • Beacon circuit breaker,
    • Gyro circuit breaker,
    • Circuit breaker lockout,
    • Aural warning horn,
    • Resettable master caution
  • Model Metal Aircraft
    • Aircraft size should be minimum 1400mmx1300mm
    • Aircraft color should be white
    • Moveable Aileron/Elevator/ Trim & Rudder
    • Aileron/elevator/trim and rudder are different color
    • DOF system should operate in sync with auto-pilot(aileron/elevator/rudder) and yoke&rudder pedal.
    • The trainer should have a beacon.
  • Remote Directional Gyro
    • Remote mounted
    • Drive signal for heading loop drive motor
    • Slaving meter drive signal
    • Original Mounted Tray
    • Shock mounted
    • Internal power supply
    • Provide’s a gyro-stabilized magnetic heading
    • Used in conjuction with the Magnetic Azimuth Transmitter.
    • Power: 14 or 28 volt dc
    • 300 degree free turnable system for testing
  • Flux Detector(The Magnetic Azimuth Transmitter)
    • Senses the direction of the earth’s magnetic field and transmits information to gyro.
  • Slaving Accessory
    • Slave/Free Gyro Switch
    • Slaving Meter indicator
    • CW/CCW Adjusment
  • Remote Control Panel
    • Heading Control
    • Altitude Control
    • Speed Control
    • Side Wings Control

 

Documentation

  • User’s Manual
  • Study Guide
  • Instructor’s Guide
  • Device’s original 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

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