Specification
The cockpit instrumentation trainer comprises the following units :
♦Flight control panel
- Electronic Flight Instrumentation Display, EFIS
- Engine Monitor System, EMS
- Three degrees of freedom instrument panel by the yoke
• Pitch movement
• Roll movement
• Yaw movement
- Flight instruments
• Turn coordinator (for electrical drive)
• Directional gyro (for electrical drive)
• Attitude indicator / Artificial horizon
• Airspeed indicator
• Altimeter
• Vertical speed indicator
- Protection of power distribution (circuit breakers)
♦ Pitot-Static System
1. Digital pressure indicator
2. Control valve
3. Pitot tube4. Static port
♦ Engine components
- 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
- Simulator mode
- Throttle control assembly
- Warning light
- Warning sound
♦ Fault simulator panel
♦ Power : AC 110V or 220V, 50Hz / 60Hz