GAA16CA388
2016-07-29 · Island Pond, Vermont, United States · None · 1 aircraft · Status: Completed
Airport 5B1
Current FAA registration · N335BE
- Make / Model
- CANADIAN LIGHT ACFT SALES &SVC BUSHCADDY EXPLORER
- Year of manufacture
- 2008 · 8 years old at event
- Engine
- ROTAX 912ULS SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 20080728
- ADS-B equipped
- Yes — Mode-S A3A880
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's exceedance of the airplane's critical angle-of-attack during approach, resulting in an inadvertent stall and hard landing.
Factual narrative
The pilot reported that he was landing in variable, gusting wind conditions and that prior to initiating the landing flare, his approach airspeed was about 45 miles per hour. About 12 feet above the runway the airplane lost lift, dropped to runway, and landed hard He recalled that the airplane impacted the runway about 150 feet from the threshold, the left landing gear partially collapsed, the airplane veered left and exited the left side of the runway, impacted a drainage culvert and nosed over. The airplane sustained substantial damage to both wings, engine mounts, and the empennage. The pilot reported that during the flight there were no mechanical malfunctions or anomalies with any portion of the airplane that would have prevented normal flight operations. As a recommendation, the pilot wrote that for the conditions he should have approached at a higher airspeed and flared further down the runway. The pilot reported that he was landing in variable, gusting wind conditions and that prior to initiating the landing flare, his approach airspeed was about 45 miles per hour. About 12 feet above the runway the airplane lost lift, dropped to runway, and landed hard He recalled that the airplane impacted the runway about 150 feet from the threshold, the left landing gear partially collapsed, the airplane veered left and exited the left side of the runway, impacted a drainage culvert and nosed over. The airplane sustained substantial damage to both wings, engine mounts, and the empennage. The pilot reported that during the flight there were no mechanical malfunctions or anomalies with any portion of the airplane that would have prevented normal flight operations. As a recommendation, the pilot wrote that for the conditions he should have approached at a higher airspeed and flared further down the runway. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Variable wind-Ability to respond/compensate
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Ability to respond/compensate
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Descent/approach/glide path-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2016_GAA16CA388.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…