NTSB Prelim: S D Martin Stallion | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-11.17.25

AirborneNextGen-
11.11.25

Airborne-Unlimited-11.12.25

Airborne-FltTraining-11.13.25

AirborneUnlimited-11.14.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Tue, May 10, 2022

NTSB Prelim: S D Martin Stallion

At An Altitude Of About 50 Ft Above Ground Level, The Engine Stopped

Location: Ridgeland, SC Accident Number: ERA22LA155
Date & Time: March 13, 2022, 15:00 Local Registration: N262KT
Aircraft: S D Martin Stallion Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Flight test

On March 13, 2022, at 1500 eastern daylight time, an experimental, amateur-built Aircraft Designs Inc. Stallion airplane, N262KT, was substantially damaged when it was involved in an accident in Ridgeland, South Carolina. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 flight test flight.

The pilot reported that the accident flight was the airplane’s 5th flight during phase 1 flight testing for the experimental amateur-built airworthiness certificate. During the takeoff roll on runway 18 at the Ridgeland Claude Dean Airport (3J1), Ridgeland, South Carolina, he noticed an amber caution message for high voltage of the No. 1 alternator on the electronic flight instrumentation system. As he raised the landing gear after liftoff, at an altitude of about 50 ft above ground level, the engine stopped. He moved the landing gear handle back to the “down” position, performed a forced landing straight ahead into an open field, and touched down about 350 yards from the departure end of the runway.

Examination of the wreckage by a Federal Aviation Administration inspector revealed that the airplane sustained substantial damage to the lower center fuselage structure.

The pilot further reported that he found the primary alternator circuit breaker open after the accident. The airplane was equipped with an experimental dual Full Authority Digital Engine Control system, which was powered by a secondary 12VDC electrical bus that included a backup battery.

The airplane was retained for further examination.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (11.14.25): Marker Beacon

Marker Beacon An electronic navigation facility transmitting a 75 MHz vertical fan or boneshaped radiation pattern. Marker beacons are identified by their modulation frequency and >[...]

Aero-News: Quote of the Day (11.14.25)

“Aviation is an incredible tool for Samaritan’s Purse. After a disaster strikes, we want people to know why we are bringing life-saving supplies. We want them to know t>[...]

Classic Aero-TV: CiES All-Digital Fuel Senders

From 2024 (YouTube Edition): New Capabilities For Business Aviation CiES Corporation President Scott Philiben walked Aero-News Editor in Chief Jim Campbell through some of what set>[...]

Airborne 11.10.25: Affordable Expo Succeeds, Citation Ascend, Kenai Shuts Down

Also: Duffy Predicts ‘Mass Chaos’, Modern Skies Coalition, More Impacts, Archer Buys Hawthorne With only a few months of preparation—and minimal outside media sup>[...]

NTSB Final Report: Lancair 320

The Experienced Pilot Chose To Operate In Instrument Meteorological Conditions Without An Instrument Flight Rules Clearance Analysis: The airplane was operated on a personal cross->[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC