EFIS-D10A Informational brochure

Product catalog summary

Introduction
The Dynon EFIS-D10A is an advanced electronic flight instrument system designed to replace traditional attitude indicators in general aviation aircraft. It meets ASTM 3153-15 standards and is STC approved for specific Cessna and Piper models.

Specifications

Weight: Main unit: 1 lb 7.4 oz; GPS-251: 7.4 oz; Backup Battery: 6.4 oz.
Connections: D-25 male connector, 1/8” NPT for plumbing, audio alarm signal.
Dimensions: 4.09”W x 3.39”H x 7.64”D.
Power: 10 - 30 Vdc, 8 watts normal, 20 watts max.
Temperature Range: -22 to 122 F (-30 to 50 C).
Screen: 3.8” diagonal.
Performance: Airspeed: 20 - 325 knots; Altitude: -1200 to 30,000 Feet; Attitude recovery from rates >150 degrees/second.
Approval: EAA STC for Cessna and Piper models.

Installation Requirements
The EFIS-D10A replaces the primary attitude indicator and requires connections to power, pitot, static, and Dynon’s GPS-251 Receiver/Antenna. Optional components include an AOA probe, remote magnetometer, and OAT. Installation may necessitate a new subpanel due to size differences.

STC Approval and Installation

Approved for installation in certain Cessna and Piper aircraft under an EAA STC.
Requires an A&P with Inspection Authorization and FAA form 337.
Allows use of commercial parts without TSO or PMA, reducing costs.

Cost and Availability
The EFIS-D10A kit starts at $2625. Installation costs vary based on installer rates and experience. The STC was available for order from EAA at Oshkosh 2016.

Features and Limitations
The EFIS-D10A offers features such as attitude, airspeed, altitude, and magnetic heading. Some features like autopilot are not approved for type certificated aircraft. It uses MEMS rate sensors and accelerometers for quick alignment and recovery.

Weight and Balance
Installation typically changes aircraft weight by less than 1 lb. Existing primary flight instruments must remain in the aircraft.

International Use
The FAA STC applies to FAA-regulated aircraft, limiting international installations.

Conclusion
The Dynon EFIS-D10A is a modern, reliable alternative to traditional attitude indicators in GA aircraft, emphasizing affordability and ease of installation.

Catalog excerpts

DYNON’S BEST-SELLING ACTUAL SIZE STC APPROVED FOR TYPE CERTIFICATED AIRCRAFT Specifications WEIGHT EFIS-D10A: 1lb 7.4oz GPS-251 for EFIS-D10A: 7.4 oz Backup Battery: 6.4 oz EDC-D10A Remote Magnetometer 3.6 oz (optional): OAT Probe (optional): 2.6 oz AOA Probe (optional): 5.7 oz Wiring Harness (optional): 9.6 oz CONNECTIONS Wiring: D-25 male connector Plumbing: 1/8” NPT (female) each for pitot, static and angle of attack Audio: Alarm signal for input to intercom or audio panel Dimensions: 4.09”W x 3.39”H x 7.64”D Voltage: 10 - 30 Vdc Power: 8 watts normal operation, 20 watts (max) if internal battery is charging Temperature: -22 to 122 F (-30 to 50 C) Screen: 3.8” diagonal Airspeed: 20 - 325 knots indicated Altitude: -1200 to 30,000 Feet Attitude: Automatic recovery from rates greater than 150 degrees per second in roll, pitch and yaw. In-flight start capability. G-Meter: -10 g’s to +10 g’s OAT: -40 to 140 F (-40 to 60 C) Approval basis: EAA STC allows for installation in Cessna 150, 152, 172, 175, 177, 182, and Piper PA-24, PA-28, PA-32, and PA-38 models, with more aircraft to follow. Your aircraft must have been equipped with a pneumatically driven attitude indicator at time of manufacture to be eligible. 19825 141st PL. NE, Woodinville, WA 98072 (425) 402-0433 • [email protected] dynonavionics.com © Dynon Avionics 2016 STC APPROVED FOR TYPE CERTI

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Frequently Asked Questions STC APPROVED FOR TYPE CERTIFICATED AIRCRAFT DYNON’S EFIS-D10A IS NOW STC APPROVED Over 15,000 experimental and light sport aircraft already fly behind Dynon products worldwide. Based on the success developing avionics for this fleet, Dynon recently partnered with EAA and FAA in the EAA’s breakthrough STC that allows installation of Dynon’s EFIS-D10A into type certificated GA aircraft. The initial STC allows the EFIS-D10A to replace the existing primary attitude indicator in many Cessna and Piper aircraft with a modern EFIS that contains no moving parts. More aircraft...

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DYNON AVIONICS EFIS-DIOA L ■ " * ® actual size EFIS-D10A now STC APPROVED for type certificated aircraft SPECIFICATIONS weight EFIS-D10A: GPS-251 for EFIS-D10A: Backup Battery: EDC-D10A Remote Magnetometer (optional): OAT Probe (optional): AOA Probe (optional): Wiring Harness (optional): Dimensions: Voltage: Power: Temperature: Screen: Airspeed: Altitude: Attitude: connections Wiring: D-25 male connector Plumbing: 1/8" NPT (female) each for pitot, static and angle of attack Audio: Alarm signal for input to intercom or audio panel G-Meter: OAT: Approval basis: 4.09"W x 3.39"H x 7.64"D 10...

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EFIS-D10A Informational brochure

EFIS-D10A Informational brochure

Catalog excerpts

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