NTSB CAROL · Event
Event FTW99LA106
Aircraft involved
Probable cause & findings
The failure of the pilot-in-command to maintain control of the airplane during the landing roll. A factor was the gusty wind conditions.
Factual narrative
On April 5, 1999, at 1020 central daylight time, a Starduster SA-100 experimental, tailwheel equipped airplane, N227FG, was substantially damaged following a loss of control while landing at the Lake Texoma State Park Airport, near Kingston, Oklahoma. The non-instrument rated private pilot, who was the owner and operator, and the sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed for the Title 14 CFR Part 91 personal flight and no flight plan was filed. The local flight originated from Kingston, Oklahoma, at 0945. The pilot reported that he maneuvered the single-place airplane to land on runway 36. Soon after touching down, the homebuilt airplane encountered "a gust of wind from the east." The right wing and empennage lifted into the air and, consequently, the nose of the airplane dragged along the runway surface approximately 30 feet. Subsequently, the airplane exited the departure end of the runway, flipped over and came to rest in the inverted position. At 1050, a weather observation facility located 25 miles northwest of the accident site reported that the winds were from 230 degrees at 15 knots with gusts to 25 knots. The pilot had accumulated a total of 1,700 flight hours at the time of the accident, of which 1,600 hours were in the make and model of the accident airplane. An FAA inspector examined the airplane and reported that the rudder was folded over the vertical stabilizer and the right wing spar was damaged. One propeller blade was separated at the propeller hub and the second propeller blade remained attached to the propeller and was "scuffed" at the tip. The pilot lost control of the airplane during the landing roll. During the landing roll a gust of wind lifted the right wing and empennage into the air and, consequently, the nose dragged along the runway surface approximately 30 feet. The airplane exited the departure end of the runway, flipped over and came to rest in the inverted position. Thirty minutes after the accident occurred a weather observation facility, located 25 miles northwest of the accident site, reported that the winds were from 230 degrees at 25 knots, gusting to 30 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_FTW99LA106.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation)
ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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