NTSB CAROL · Event
Event LAX05CA081
Aircraft involved
Probable cause & findings
the pilot's misjudged flare, which resulted in a stall and a hard landing.
Factual narrative
On January 30, 2005, about 1540 Pacific standard time, a Cessna 182P, N9003M, landed hard at Reno/Tahoe International Airport, Reno, Nevada. Comstock Aviation, Inc., was operating the airplane under the provisions of 14 CFR Part 91. The private pilot and three passengers were not injured; the airplane sustained substantial damage. The personal cross-country flight departed Minden-Tahoe Airport, Minden, Nevada, about 1430, with the planned destination of Reno. Visual meteorological conditions prevailed, and a flight plan had not been filed. In a telephone interview with a National Transportation Safety Board investigator, the pilot reported flying in the traffic pattern for runway 16L at Reno. Established in the base leg portion of the traffic pattern, the pilot stated that the airplane's indicated airspeed was about 85 knots and the flaps were positioned at 20 degrees. After turning onto the final approach segment, the pilot slowed the airplane to 80 knots, and configured the airplane with 40 degrees of flaps. The pilot did not recall the indication of the precision approach path indicator lights (PAPI) during the approach but opined that the glidepath was normal. Crossing the runway threshold at 70 knots, the pilot reduced power and initiated the transition from approach to a landing attitude. He said that the airplane stalled above the runway and touched down hard on the main landing gear. The airplane began to porpoise and bounced twice before settling into the landing rollout. The pilot reported that after exiting the airplane, he noted that the propeller had struck the runway during landing, and the landing nose gear tire was flat. The pilot reported no preimpact mechanical malfunctions or failures with the airplane. A Federal Aviation Administration inspector examined the airplane after the accident. The inspector noted that the damage to the airplane included a collapsed nose landing gear strut and deformation to the firewall. The airplane landed hard and porpoised, resulting in a collapse of the nose gear strut and deformation to the firewall. After turning onto the final approach segment, the pilot slowed the airplane to 80 knots and configured the airplane with 40 degrees of flaps. Crossing the runway threshold at 70 knots, the pilot reduced power and initiated the transition from approach to a landing attitude. The airplane stalled above the runway and touched down hard on the main landing gear. The airplane began to porpoise and bounced twice before settling into the landing rollout. The pilot reported that there were no preimpact mechanical malfunctions or failures. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_LAX05CA081.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…
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