EFIS And EICAS Trainer

The system combines primary flight instrumentation, aircraft systems instrumentation, engine instrumentation, warnings/alerts, and navigational information, all displayed on two LCD color screens. The EFIS / EICASTrainer is based on panel-mount LCD flight and navigation displays. There are separate PFD and MFD screens, with fullreversionary backup for redundancy. This is an advanced technology avionicssuite designed to integrate pilot/aircraft interaction into one central system. The trainer has a full functional primary flight display (PFD) for attitude/directionalguidance with electronic engine monitoring and detailed moving-map multifunction display (MFD) capabilities. The is a complete packaget hat represents EFIS / EMS / EICAS displaying flight instrumentation, position,navigation, communication, and identification information to the pilot using dual 7 wide (800 x 480) flat-panel color displays.

Magnetometer:
This unit receives power directly from theAHRS and communicates with it via an RS-485 digital interface. Magnetome terme a sures the local magnetic field and sends data to the AHRS for processing to determine aircraft magnetic heading.
Autopilot Interface:
With the Integrated Autopilot configured, the system issues pitch and roll steering commands to the external autopilot unit. The can also communicate with various third-party external autopilot units. 
Outside Air Temperature (OAT) Probe:
The Temperature Probe provides raw air temperature data.
Power: 110V AC or220V AC at 60/50 Hz, single phase.