NTSB CAROL · Event
Event SEA98LA117
Registry · N92519
FAA Aircraft Registry record.
Make / Model
CESSNA 182N
Year of manufacture
1970 · 28 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19980423
ADS-B equipped
Yes — Mode-S ACD35A
Registrant of record
FLORY AIR LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Directional control was not maintained. A wet runway surface was a factor.
Factual narrative
On July 2, 1998, at 1930 mountain daylight time, a Cessna 182N, N92519, registered to and operated by Interstate Aviation as a 14 CFR Part 91 personal flight, ran off the side of the airstrip at Big Creek, Idaho, and collided with a fence. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airplane was substantially damaged and the private pilot and one passenger were not injured. The other two passengers received minor injuries. The flight had originated from Lewiston, Idaho, about one hour prior to the accident. In a written statement, the pilot reported that he over flew the runway twice before setting up an approach to runway 19. The pilot stated that he was high on the final approach and slipped the airplane to descend. The airplane landed within the first 1/3 of the length of the runway in a full stall on the main landing gear. The pilot stated that the touch down was on the left side of centerline due to cones that were placed on the airstrip. The pilot reported that from the point of touchdown to impact with the fence, the airplane was gradually sliding to the left. The pilot tried to correct with right rudder control and braking action, however, the airplane continued to the left and collided with a fence. The pilot stated that the airstrip surface (grass) was wet and rougher than what he remembered from previous flights into this airstrip. The pilot reported that there were no mechanical failures or malfunctions with the airplane at the time of the accident. The Big Creek Airstrip is 3,550 feet in length with a turf surface. Landing is recommended to the south. The pilot reported that he over flew the airstrip twice before setting up for final approach. The pilot stated that while on final approach, the airplane was high so he slipped the airplane to descend. The airplane landed within the first 1/3 of the length of the airstrip in a full stall on the main landing gear. The pilot stated that the touch down was on the left side of the centerline due to cones that were placed on the airstrip. The pilot reported that from the point of touchdown to impact with the fence, the airplane was gradually sliding to the left. The pilot tried to correct with right rudder control and braking action, however, the airplane continued to the left and collided with a fence. The pilot reported that the grass airstrip was wet and that the surface was rougher than what he had remembered from previous flights into the airstrip. The pilot reported that there were no mechanical failures or malfunctions with the airplane at the time of the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_SEA98LA117.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 ↗