EFD-750 | Electronic Flight Display

Product overview

The compact EFD-750 is a scalable OEM and retrofit solution that comes standard with attitude, airspeed, altitude and slip/skid. Customized hardware configurations are available to support internal or external air data from an existing digital source on the aircraft. EFD-750 also reduces maintenance time by storing all display and interface configuration data in an OEM or installer-programmed data configuration module.

The EFD-750 is compatible with existing digital navigation and GPS receivers and features configurable airspeed VNE and VMO warning cues for Part 23, Part 25 and Part 27/29 aircraft.

Key features

Hardware

Active-matrix liquid crystal display with 3.5" diagonal viewable area
Rotary knob to adjust altimeter and to scroll and select menu options
Ambient light sensor to automatically adjust brightness
Solid state internal sensors for attitude, rates and acceleration
Pilot/static inputs, or digital air data computer inputs for airspeed, altitude, and Mach
Optional interface to MAG-500 for heading information
MicroSD card slot on front bezel for field-loadable software and configuration updates
Dimensions: 3.125" round case, 5.62" deep case behind panel (+0.66 connector)

Flight crew display

Attitude and slip/skid
Altitude, airspeed, and Mach
Heading or track – (Optional)
GPS and/or VOR/ILS navigation (Optional)

Pilot menu options

The pilot menu list includes:

NAV mode (VOR/ILS, GPS, Off)

When nav is enabled:

Set sourse (When VOR/ILS)
Course direct-to (When VOR)
Data field on/off

When data fields are enabled:

Set display brightness
BARO type (In, hPa, Mb)
BARO sync

When configured for baro sync is enabled:

Metric altitude on/off

When configured for metric is enabled:

Attitude alignment
System status

Specifications

Weight and design	Maximum 2.75 lb./1.25 kg DO-178C and DO-254 - Design Assurance Level A
Interfaces	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
Power	14 or 28 VDC electrical systems (10-32 VDC)
Navigation	VOR/ILS or GPS Navigation or both
TSO	C106, C113a, C201, C209
ETSO	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"
Certification	Technical Standard Orders (TSO): TSO-C106 Air Data Computer TSO-C113a Airborne Multi-Function Displays TSO-C201 Attitude and Heading Reference System (AHRS) TSO-C209 Electronic Flight Instrument System (EFIS) Display Software & Firmware: EFD-750: Software, DO-178C Level A \| Hardware, DO-254 Level A MAG-500: Hardware: DO-254 Level C

Downloads

EFD-750 Brochure

PDF875.9 KB

Avionics for Helicopters Brochure

PDF1.4 MB

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EFD-750 Electronic Flight Display