CEN25FA014

NTSB accident investigation · Rans S12 · Church Point, LA · October 15, 2024

Accident · FatalClass 3 · FieldPreliminary report
Date
October 15, 2024, 15:14 local (20:14 UTC)
Place
Church Point, LA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N912RSRans S12
Defining event
Approach-VFR pattern base: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Investigation ongoing
Investigation class
Class 3
NTSB office
Central Region
Parties
Federal Aviation Administration, Baton Rouge FSDO
FAA report
20241015016919A
Case key
195321

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Preliminary report

What NTSB knew early in the investigation. It may change in the final report.

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.

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Aircraft

Registration
N912RS
Reported as
Rans S12 (S)
Category
Airplane
Serial number
06000922
Built
2010
Damage
Destroyed
Flight
Flight test · Part 91
Airworthiness certificate
Special, Experimental (Special)
Destination
Same as departure
Airport
Private, runway 04, grass/turf

Weather

Conditions
Visual (VMC) · Day
Wind
20° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
86 °F, dew point 63 °F
Altimeter
29.95 inHg
Observed at
OPL, 10 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.