NTSB CAROL · Event
Event DEN01LA031
Registry · N2386C
FAA Aircraft Registry record.
Make / Model
CESSNA R182
Year of manufacture
1978 · 22 years old at event
Engine
LYCOMING 0-540 SERIES (250 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19780213
ADS-B equipped
Yes — Mode-S A22965
Registrant of record
SUITER THOMAS D
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the flight instructor's inadequate supervision of the dual student, which resulted in a hard landing. Contributing factors were the dual student flaring the airplane prematurely, resulting in an inadvertent stall/mush.
Factual narrative
On December 13, 2000, at 1158 mountain standard time, a Cessna R182, N2386C, operated by McAir Aviation, Inc., was destroyed during a hard landing at Jeffco Airport, Broomfield, Colorado. The commercial certificated flight instructor and her private certificated student were not injured. Visual meteorological conditions prevailed at the time, and no flight plan had been filed for the instructional flight being operated under Title 14 CFR Part 91. The flight originated at Pueblo, Colorado, appoximately 45 minutes before the accident. According to the accident report submitted by the flight instructor, they were cleared to land on runway 11L. Despite the wind "shifting directions," proper wind correction was applied and the airplane landed. During the rollout, the nose started shaking and full up elevator was applied. The propeller struck the ground and the airplane came to a halt. According to the airplane owner who witnessed the accident, the airplane "was too high for normal glidepath...the plane suddenly descended in a near level flight attitude from an altitude of approximately 40 feet above the runway...the plane hit in a full stalled configuration." Postaccident inspection revealed the airframe was extensively damaged, particularly around the cabin doors when the main landing gear was driven up into the fuselage. The airplane was subsequently declared to be a total loss. The airplane was cleared to land on runway 11L. The flight instructor said that despite the wind 'shifting directions,' correct wind correction was applied and the airplane landed. During the rollout, the nose started shaking and full up elevator was applied. The propeller struck the ground and the airplane came to a halt. But according to the airplane owner who witnessed the accident, the airplane 'was too high for normal glidepath...the plane suddenly descended in a near level flight attitude from an altitude of approximately 40 feet above the runway...the plane hit in a full stalled configuration,' which drove the landing gear into the fuselage. The airplane was destroyed. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_DEN01LA031.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 ↗