Cockpit Instrumentation Trainer

Three degrees of freedom instrument panel permits full demon stration of attitude and directional gyro functions. The Cockpit Instrumentation System with Electronic Flight Instruments and electronic engine display. 

Standard Features:
Functional engine monitoring system connected to engine sensors
Provision of engine sensor simulation
Functional digital primary flight display mounted on a panel that can simulate roll,pitch, and yaw movements controlled by a mechanism operated by a control yoke.
Functional pitot- static system with provision for conducting pitot static system checks
Standby Instruments installed.

The Model is fitted with the following sensors:
EGT  Thermo couples(Qty. 4)
CHT Thermo couples (Qty. 4)
Oil Temperature Sensor
OAT Sensor
Pitot-static Tube
Fuel Flow Sensor
Manifold Pressure Sensor
Fuel Pressure Sensor
Engine RPM Sensor
Fuel Level Sensor
Ammeter Shuntv
Oil Pressure Sensor.