Specification

The cockpit instrumentation trainer comprises the following units :

♦Flight control panel

1. Electronic Flight Instrumentation Display, EFIS
2. Engine Monitor System, EMS
3. Three degrees of freedom instrument panel by the yoke 
   • Pitch movement
   • Roll movement
   • Yaw movement
4. Flight instruments
   • Turn coordinator (for electrical drive)
   • Directional gyro (for electrical drive)
   • Attitude indicator / Artificial horizon
   • Airspeed indicator
   • Altimeter
   • Vertical speed indicator
5. Protection of power distribution (circuit breakers)

♦ Pitot-Static System
1. Digital pressure indicator
2. Control valve
3. Pitot tube4. Static port

♦ Engine components

1. 1. Actual mode 
   • Cylinder Head Temperature (CHT) thermocouple
   • Exhaust Gas Temperature (EGT) thermocouple
   • Outside Air Temperature (OAT) sensor
   • Fuel pressure sensor
   • Oil pressure sensor
   • Oil temperature sensor
   • Fuel quantity sensor
2. Simulator mode
3. Throttle control assembly
4. Warning light
5. Warning sound

♦ Fault simulator panel

♦ Power : AC 110V or 220V,  50Hz / 60Hz