GAA16CA050
2015-11-13 · Bowstring, Minnesota, United States · None · 1 aircraft · Status: Completed
Airport 9Y0
Aircraft involved
Probable cause & findings
The pilot exceeded the critical angle of attack during takeoff which resulted in an aerodynamic stall and impact with a wind sock and terrain.
Factual narrative
The pilot reported that while taking off with 20 degrees of flaps from a grass airstrip, the airplane rotated about 50 knots and climbed to an altitude of about 80 feet above the ground. The pilot reported that the airplane "seemed" not to be "making" enough power to continue to climb. The pilot elected to abort the takeoff and land directly ahead on what remained of the landing strip. While landing the airplane impacted a wind sock located about 140 feet to the left of centerline and about 500 feet short of the departure end of the runway on the left edge of the landing strip, which resulted in substantial damage to the firewall. In a telephone interview with the NTSB Investigator-in-charge (IIC) the pilot stated that the stall warning horn was audible during the initial climb. The pilot reported that while taking off with 20 degrees of flaps from a grass airstrip, the airplane rotated about 50 knots and climbed to an altitude of about 80 feet above the ground. The pilot reported that the airplane "seemed" not to be "making" enough power to continue to climb. The pilot elected to abort the takeoff and land directly ahead on what remained of the landing strip. While landing the airplane impacted a wind sock located about 140 feet to the left of centerline and about 500 feet short of the departure end of the runway on the left edge of the landing strip, which resulted in substantial damage to the firewall. In a telephone interview with the NTSB Investigator-in-charge (IIC) the pilot stated that the stall warning horn was audible during the initial climb. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Aircraft capability-Climb capability-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded - C
Verbatim from NTSB's published report. Source file
NTSB_2015_GAA16CA050.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- 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 …
- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…