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-12.08.25

AirborneNextGen-
12.09.25

Airborne-Unlimited-12.10.25

Airborne-AffordableFlyers-12.11.25

AirborneUnlimited-12.12.25

AFE 2025 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

Aero-News: Quote of the Day (12.09.25)

“We respectfully call on the City of Mesa to: 1. Withdraw the landing fee proposal immediately 2. Engage with the aviation community before making decisions that impact safet>[...]

ANN's Daily Aero-Term (12.09.25): High Speed Taxiway

High Speed Taxiway A long radius taxiway designed and provided with lighting or marking to define the path of aircraft, traveling at high speed (up to 60 knots), from the runway ce>[...]

ANN's Daily Aero-Linx (12.09.25)

Aero Linx: International Federation of Airworthiness (IFA) IFA uniquely combines together all those with responsibility for policies, principles and practices concerned with the co>[...]

NTSB Final Report: Diamond Aircraft Ind Inc DA20C1 (A1); Robinson Helicopter R44

Controller’s Expectation That VW02 Would Have Departed Sooner Led To An Inadequate Scan And Loss Of Situational Awareness Analysis: A Robinson R-44 helicopter N744AF, VW02 (V>[...]

ANN FAQ: Q&A 101

A Few Questions AND Answers To Help You Get MORE Out of ANN! 1) I forgot my password. How do I find it? 1) Easy... click here and give us your e-mail address--we'll send it to you >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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