NTSB CAROL · Event
Event FTW97LA211
Aircraft involved
Probable cause & findings
The pilot's impairment of judgment and performance due to alcohol which led to an attempted takeoff in an airplane without an elevator installed.
Factual narrative
On June 6, 1997, at 2350 central daylight time, a Beech 58 airplane, N22SS, registered to Global Aircraft Company, was stolen and substantially damaged during an attempted takeoff at Wiley Post Airport near Oklahoma City, Oklahoma. Visual meteorological conditions prevailed, and a flight plan was not filed. The pilot and his one passenger sustained minor injuries. The flight was originating at the time of the accident. During the takeoff roll the airplane overran the departure end of runway 17L. The aircraft traveled 600 to 800 feet impacting the localizer antenna and continued approximately 100 feet impacting the airport perimeter fence. It continued across a ditch and road coming to rest 50 feet south of the road. Examination of the airplane by the FAA inspector revealed that the nose landing gear and the main landing gear were collapsed, and the leading edges of both wings were damaged. Further examination of the airplane revealed that the elevator was missing. The owner reported that he was having the airplane refurbished, and the elevator had been removed for painting on June 1, 1997. The toxicology report from Baptist Medical Center of Oklahoma, Oklahoma City, Oklahoma, revealed 0.180 percent alcohol was detected in the pilot's blood. This specimen was take on June 7, 1996, about one hour 12 minutes after the accident. See the enclosed lab report. According to the FAA inspector, the pilot's commercial certificate was revoked seven years prior for stealing an airplane. According to the owner the pilot and passenger were not authorized to use the airplane. Attempts to obtain a completed Pilot/Operator Report, NTSB Form 6120.1/2, were unsuccessful. During the takeoff roll the airplane overran the departure end of the runway. The aircraft traveled 600 to 800 feet impacting the localizer antenna, and continued approximately 100 feet impacting the airport perimeter fence. It continued across a ditch and road coming to rest 50 feet south of the road. Examination of the airplane revealed that the elevator was not installed. According to the owner, he was having the airplane refurbished, and the elevator had been removed for painting on June 1, 1997. According to blood samples taken at the hospital about one hour 12 minutes after the accident, the pilot had a blood alcohol concentration of 180 mg/dl. The pilot and passenger were not authorized by the owner to use the airplane. The pilot's commercial certificate was revoked seven years prior for stealing an airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_FTW97LA211.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 (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2011 · Conference Paper
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- NASA NTRS 2019 · Other
Documentation for Three Wake Vortex Model Data Sets from Simulation of Flight 587 Wake Vortex Encounter Accident Case
This document contains a general description for data sets of a wake vortex system in a turbulent environment. The turbulence and thermal stratification of the environment are representative of the co…
- NASA NTRS 2016 · Conference Paper
An overview of SAE ARP 1587: Aircraft gas turbine engine monitoring system guide
A systematic approach to developing an engine monitoring system (EMS) is outlined. An extensive shopping list of EMS capabilities and benefits are included.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
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