NTSB CAROL · Event
Event ERA10CA304
Registry · N5075K
FAA Aircraft Registry record.
Make / Model
CESSNA 305A
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19820122
ADS-B equipped
Yes — Mode-S A65702
Registrant of record
CELEBRATE FREEDOM FOUNDATION
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot-in-command's loss of airplane control during landing, which resulted in a ground-loop.
Factual narrative
According to the pilot-in-command (PIC), after touchdown, a gust of wind pushed the tailwheel-equipped airplane towards the left side of the runway. In an attempt to correct the drift, he applied right rudder and right brake. The check pilot, seated in the rear, added power which resulted in a ground loop. The airplane continued its turn, about 150 feet off of the runway surface, until the left main landing gear dug into the ground and sheared off. According to the check pilot, as the airplane crossed the end of the runway, on heading and about 5 knots above a stall, the wind shifted to the airplane's port quarter, with gusts up to 30 knots. The airplane stalled, and "dropped to the runway with a rapid sink rate." The check pilot attempted to advise the PIC to go around "by adding power, but he thought I wanted control of the plane and threw up his hands and said, 'You got it!'" By that time, the airplane was off the right side of the runway, "in the sand and no one in control." According to the pilot-in-command (PIC), after touchdown a gust of wind pushed the tailwheel-equipped airplane toward the left side of the runway. In an attempt to correct the drift, he applied right rudder and right brake. The check pilot, seated in the rear, added engine power, which resulted in a ground loop. The airplane continued its turn, about 150 feet off of the runway surface, until the left main landing gear dug into the ground and sheared off. According to the check pilot, as the airplane crossed the end of the runway, about 5 knots above stall speed, the wind shifted, with gusts up to 30 knots. The airplane stalled and descended to the runway with a rapid sink rate. The check pilot advised the PIC to go around and instructed him to add engine power. The check pilot further stated that the PIC thought that he wanted the check pilot to take control of the airplane and raised his hands off the controls and said, "You got it!." By that time, the airplane was off the right side of the runway in the sand with neither pilot at the controls. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Action/decision-Action-Incorrect action performance-Instructor/check pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Not specified
- — Environmental issues-Conditions/weather/phenomena-Wind-Sudden wind shift-Not specified
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA10CA304.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 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…
Browse the full corpus — academia portal ↗