FTW02LA231
2002-08-06 · Welsh, Louisiana, United States · Minor · 1 aircraft · Status: Completed
Airport 6R1
Aircraft involved
Probable cause & findings
the pilot's failure to maintain the minimum required airspeed for flight, which resulted in an inadvertent stall.
Factual narrative
On August 6, 2002, at 1600 central daylight time, a Page Rans S-7 amateur-built airplane, N497RP, was substantially damaged when it impacted terrain during takeoff from the Welsh Airport, Welsh, Louisiana. The airplane was registered to and operated by the pilot. The private pilot, sole occupant of the airplane, sustained minor injuries. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight was originating at the time of the accident and was destined for the Jennings Airport, Jennings, Louisiana. The 386-hour pilot reported that during a normal takeoff to the north from a turf covered runway, the airplane stalled, and subsequently, impacted the ground. He added that at the time of the accident, the wind was from the north at 10 knots gusting to 15 knots. According to initial responders to the accident site, the airplane's left wing was "destroyed," and the landing gear separated from the airplane. Additionally, the engine was displaced aft beneath the airplane's fuselage. During a normal takeoff to the north from a turf covered runway, the airplane stalled, and subsequently, impacted the ground. The pilot reported that at the time of the accident the wind was from the north at 10 knots gusting to 15 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_FTW02LA231.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
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- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…