NTSB CAROL · Event
Event FTW97LA004
Aircraft involved
Probable cause & findings
Loss of control when the pilot exceeded the velocity of stall while in a turn.
Factual narrative
On October 4, 1996, at 1240 mountain daylight time, a PDPS PZL-Bielsko SZD-59 glider, N597R, impacted the ground after entering uncontrolled flight while in the traffic pattern at Sterling Municipal Airport, Sterling, Colorado. The commercial pilot received fatal injuries and the aircraft sustained substantial damage. Visual meteorological conditions prevailed for this local area personal flight operating under Title 14 CFR Part 91 and no flight plan was filed. The flight departed Sterling, approximately 20 minutes prior to the accident. According to witnesses, the pilot had been practicing in the aerobatics area and was in the process of returning to the airport for landing. An eyewitness said that the tow plane landed on runway 33 and began back taxiing. The glider then came down the runway about 100 feet above ground level, wings level, and entered a left turn at bout 45 degrees angle of bank. The witness said the nose began to drop and the bank angle increased to about 60 degrees. The glider then dove into the ground beside the runway at approximately 60 degrees nose down attitude. The witness said the glider came to rest in an upright position facing to the south. The terrain around the runway was flat grass covered farm fields. An examination of the glider by an FAA airworthiness inspector provided no evidence of preimpact failure or malfunction. According to the flight manual for the aircraft, the minimum speed marking on the airspeed indicator is 51 knots (59 mph). This speed is 1.1 X Vs (velocity of stall), wings level, at the maximum gross weight approved for aerobatics. Accelerometer limits are +7 and -5. Stall/spin recovery requires a maximum of 623 feet loss of altitude for recovery. While returning to land after a practice aerobatics flight, the pilot flew the glider down the runway of intended landing at 100 feet above ground level and then entered a 45 degree bank left turn. The nose began to drop and the bank angle increased to about 60 degrees and the glider dove into the ground next to the runway with a nose attitude of approximately 60 degrees nose down. At the time, the glider tow plane was back taxiing on the runway. Terrain around the airport was flat grass covered farm fields. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_FTW97LA004.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 (icing, stall, 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.
- 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.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- 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…
- NASA NTRS 2019 · Conference Paper
Simulation Modeling Requirements for Loss-of-Control Accident Prevention of Turboprop Transport Aircraft
In-flight loss of control remains the leading contributor to aviation accident fatalities, with stall upsets being the leading causal factor. The February 12, 2009.
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP)
NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
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