EFD-750 ELECTRONIC FLIGHT DISPLAY
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Catalog excerpts

EFD-750 ELECTRONIC FLIGHT DISPLAY - 1

BANNER PLACEHOLDER CLICK IN THIS RECTANGLE AND THEN GO TO FILE -> PLACE TO INSERT IMAGE EFD-750 ELECTRONIC FLIGHT DISPLAY Compact, high-performance electronic flight display. KEY FEATURES • Mirrors PFD presenting airspeed, altitude, attitude and slip data • Options for heading and navigation • Certified to DO-178C and DO-254 Level A • Compatible with existing digital NAV and GPS receivers • High-resolution, 24-bit color display • 3" round case for easy installation into existing panel cutouts L3Harris’ next generation EFD-750 Electronic Flight Display is one of the most advanced backup systems designed specifically for turboprop, light jet and helicopter platforms. Compatible with existing digital navigational displays and GPS receivers, the EFD-750 is a configurable solution which provides pilots with a clear, high-resolution view mirroring the Primary Flight Display presenting airspeed, altitude, attitude and slip data. The heading display is available through an existing digital heading source, or an optional low cost and compact MAG-500 magnetometer. It also provides night vision capabilities through a green-lit bezel providing pilots better situational awareness. The EFD-750 utilizes an OEM or installer programmed data configuration module that stores all display and interface configuration data. VMO warning cues for Part 23, Part 25 and Part 27/29 aircraft • Configurable Static Source Error Correction (SSEC) and Total Source Error Correction (TSEC) for pressure altitude and calibrated airspeed corrections • Barometric Altimeter settings may be synchronized to the aircraft’s primary display system to reduce pilot actions • Supports night vision capabilities through ambient LEDs

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EFD-750 ELECTRONIC FLIGHT DISPLAY - 2

SPECIFICATIONS Pack 50 years of standby experience in your panel. EFD-750 Weight: ARINC 429 Inputs (5), ARINC 429 Output (1), RS-485 Serial Input (interfaces with MAG-500)(1), Analog Input (OAT) (1), Dimming Bus (1), I2C interface to the DCM-750 (1). Dimming Bus input is configurable as 5V, 14V, or 28V. VOR/ILS or GPS Navigation or both No ETSO marking on the Articles are required in accordance with FAA/EASA Technical Implementation Procedure (TIP) Rev 6 paragraph 3.3.3 “TSO/ETSO Articles”. DO-178C and DO-254 - Design Assurance Level A TECHNICAL STANDARD ORDERS (TSO) TSO-C106 – Air Data...

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