NTSB CAROL · Event
Event FTW97LA082
Aircraft involved
Probable cause & findings
The pilot's failure to maintain control during takeoff.
Factual narrative
On January 14, 1997, approximately 1230 central standard time, a Garrett Baby Great Lakes homebuilt experimental bi-plane (tail wheel), N1030G, was substantially damaged following a loss of control during take off, from West Texas Airport, El Paso, Texas. The commercial pilot, the sole occupant and owner, received minor injuries. No flight plan was filed and visual meteorological conditions prevailed for the personal flight conducted under Title 14 CFR Part 91. The pilot reported that after a normal run-up at the hold short line, he taxied onto the runway and lined up on centerline for take off. With the "stick just forward of neutral, and maintaining directional control with rudders", he slowly added power and began his take off roll. As the tail wheel lifted off the ground, he "went to full power (2,500 RPM)." Subsequently, the airplane began to slide sideways toward the left side of the runway, and just as flying airspeed was attained, the aircraft "began to porpoise." After departing the runway surface, the airplane struck a fence and a sand dune, coming to rest inverted. According to the pilot, the entire event took about 5-10 seconds, and the airplane traveled 500 feet. The pilot/owner reported no mechanical problems with the aircraft. The aircraft sustained structural damage to the upper and lower left wings. The pilot reported that after a normal run-up at the hold short line, he taxied onto the runway and lined up on centerline for takeoff. With the 'stick just forward of neutral, and maintaining directional control with rudders', he slowly added power and began his takeoff roll. As the tail wheel lifted off the ground, he 'went to full power (2,500 RPM).' Subsequently, the airplane began to slide sideways toward the left side of the runway, and just as flying airspeed was attained, the aircraft 'began to porpoise.' After departing the runway surface, the airplane struck a fence and a sand dune, coming to rest inverted. According to the pilot, the entire event took about 5-10 seconds, and the airplane traveled 500 feet. The pilot/owner reported no mechanical problems with the aircraft. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_FTW97LA082.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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