Features:

1. Indicators operate in sync with auto-pilot system
2. Aircraft position controlled by yoke.
3. 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.
4. 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.
5. Automatic/Motorized Throttle Lever
6. Yoke and rudder pedal can move the control surfaces of the aircraft.
7. Servos operate in sync with auto-pilot and yoke/rudder pedal.
8. 2 axis DOF + 1 DOF system
9. Pitch Trim Servo System
10. Heading Feed Back
11. Altitude Feed Back
12. Active Remote Gyro HSI System
13. Remote Control Panel
14. Vacuum Pump
15. Remote Altitude control & feedback
16. Remote Heading control & feedback
17. Remote side wing control
18. Remote head wing control
19. The aircraft automatically calibrated to runway position when the trainer is turned on.
20. Instructor’s panel for Fault Insertion

Components:

1. 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)
2. Yoke (Automatic/Motorized)
3. Rudder Pedal (Automatic/Motorized)
4. Throttle Control (Automatic/Motorized)
5. Pitch / Yaw / Roll / Pitch Trim servos
6. 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.
7. 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
8. 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.
9. Remote Directional Gyro
   • Remote mounted
   • Drive signal for heading loop drive motor
   • Slaving meter drive signal
   • Original Mounted Tray
   • Shock mounted
   • internal power supply
   • Provides a gyro-stabilized magnetic heading
   • Used in conjunction with the Magnetic Azimuth Transmitter.
   • Power: 14- or 28-volt dc
   • 300-degree free turn able system for testing
10. Flux Detector (The Magnetic Azimuth Transmitter)
    • Senses the direction of the earth’s magnetic field and transmits information to gyro
11. Slaving Accessory
    • Slave/Free Gyro Switch
    • Slaving Meter indicator
    • CW/CCW Adjustment
12. Remote Control Panel
    • Heading Control
    • Altitude Control
    • Speed Control
    • Side Wings Control