Rans S12 N912RS

Summary

On 15 October 2024 at about 20:14 local time, a Rans S12 registered N912RS was involved in an accident near Church Point, Louisiana, United States. One person was on board and one died. The aircraft was destroyed. No probable cause has been published yet; this accident is still under investigation.

Date

15 October 2024 at 20:14

Classification

Accident

Location

Church Point, Louisiana, United States

Nearest airport

Private

Coordinates

30.4178, -92.2437

Aircraft

Rans S12

Registration

N912RS

Category

Airplane

Year built

2010

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Flight Test

Phase of flight

Not recorded

Aircraft damage

Destroyed

Weather

VMC

Light

Day

NTSB number

CEN25FA014

1 person died.

The NTSB has not published a probable cause for this record. The investigation is still open; a final report usually follows one to two years after the accident.

Nothing about the cause is stated here that is not in the source record.

Read the full NTSB narrative

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.

Quoted verbatim from the NTSB record.