NTSB Prelim: RANS S12 | 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-04.21.25

Airborne-NextGen-04.22.25

AirborneUnlimited-04.23.25

Airborne-FltTraining-04.24.25

AirborneUnlimited-04.25.25

Tue, Nov 05, 2024

NTSB Prelim: RANS S12

During The Turn From The Base Leg To The Final Leg Of The Approach, The Airplane Snapped Over And Entered An Aerodynamic Spin

Location: Church Point, LA Accident Number: CEN25FA014
Date & Time: October 15, 2024, 15:14 Local Registration: N912RS
Aircraft: RANS S12 Injuries: 1 Fatal
Flight Conducted Under: Part 91: General aviation - Flight test

On October 15, 2024, at 1514 central daylight time, a Rans S12S, N912RS, was involved in an accident near Church Point, Louisiana. The airline transport pilot sustained fatal injuries. The airplane was destroyed. The airplane was operated under Title 14 Code of Federal Regulations as a Part 91 maintenance test flight.

The airplane had not flown for about three years before it was purchased by the current owner whose intent was to learn how to fly using the accident airplane. The airplane owner, the pilot, and two other individuals performed maintenance on the airplane during the previous two months in preparation for the test flight that was flown by the pilot. During the test flight, the pilot performed maneuvers that included aerodynamic stalls, steep turns, and glide ratios. The pilot reported via radio that there were no issues with the airplane, and it was outstanding in its flying. The pilot then reported that he was returning to the departure airstrip. The airplane entered a downwind landing followed by a base leg for landing. During the turn from the base leg to the final leg of the approach, the airplane snapped over and entered an aerodynamic spin. The airplane descended while spinning and the engine sound increased and then decreased, which was consistent with an application followed by a reduction of engine power. 

The airplane impacted a field and was destroyed by impact forces. Postaccident examination of the airplane revealed no mechanical malfunction/failure that would have precluded normal airplane operation. The airplane was not equipped nor was it 
required to be equipped with a stall warning system due its experimental categorization.

The wreckage was recovered to a secure location for further examination. 

FMI: www.ntsb.gov

Advertisement

More News

Aero-News: Quote of the Day (04.24.25)

"This enables all parts of the digital portfolio to focus on their strengths. Our commitment to meeting our customers' needs is unwavering as we move forward with our core products>[...]

ANN's Daily Aero-Linx (04.24.25)

Aero Linx: National Aeronca Association We are dedicated to supporting the design and preserving the history of Aeronca aircraft. Founded by Jim Thompson and fostered by his leader>[...]

NTSB Final Report: Cessna 180

Pilot’s Failure To Maintain Clearance From The Water During A Low Pass Over A Lake Analysis: The pilot reported that he descended to make a low pass over Pettit Lake. He note>[...]

ANN's Daily Aero-Term (04.24.25): Downburst

Downburst A strong downdraft which induces an outburst of damaging winds on or near the ground. Damaging winds, either straight or curved, are highly PCG D−3 Pilot/Controller>[...]

Airborne-Flight Training 04.24.25: GA Refocused, Seminole/Epic, WestJet v TFWP

Also: Cal Poly Aviation Club, $$un Country, Arkansas Aviation Academy, Teamsters Local 2118 In response to two recent general aviation accidents that made national headlines, more >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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