The EFIS / EICASTrainer is based on panel-mount LCD flight and navigation displays. 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. 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 system combines primary flight instrumentation, aircraft systems instrumentation, engine instrumentation, warnings/alerts, and navigational information, all displayed on two LCD color screens. 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.
Magnetome terme a sures the local magnetic field and sends data to the AHRS for processing to determine aircraft magnetic heading. This unit receives power directly from theAHRS and communicates with it via an RS-485 digital interface.
Outside Air Temperature (OAT) Probe:
The Temperature Probe provides raw air temperature data.
The can also communicate with various third-party external autopilot units. With the Integrated Autopilot configured, the system issues pitch and roll steering commands to the external autopilot unit.
110V AC or220V AC at 60/50 Hz, single phase.