Features:

1. Indicators operate in sync with auto-pilot system
2. Aircraft position controlled by yoke.
3. Yoke and rudder pedal can move the control surfaces of the aircraft.
4. Servos operate in sync with auto-pilot and yoke.
5. 2 axis DOF + 1 DOF system
6. The aircraft automatically calibrated to runway position when the trainer is turned on.
7. 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 (Auto-Centered)
3. Rudder Pedal
4. Throttle Control
5. Pitch / Yaw / Roll 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,
   • 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 & Rudder
   • Aileron/elevator 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.