NTSB CAROL · Event
Event SEA98LA185
Registry · N4DX
FAA Aircraft Registry record.
Make / Model
CESSNA 210L
Year of manufacture
1972 · 26 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
20030917
ADS-B equipped
Yes — Mode-S A4A850
Registrant of record
HUFFMAN AVIATION & EQUIPMENT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain adequate airspeed which resulted in a stall/mush. Factors include allowing his attention to be diverted by what he perceived to be a lateral control problem.
Factual narrative
On September 21, 1998, approximately 1700 Pacific daylight time, an experimental Duncan DX4, N4DX, impacted the terrain just after the pilot initiated the turn from downwind to base at Priest River Municipal Airport, Priest River, Idaho. The private pilot, who was the sole occupant, received serious injuries, and the aircraft, which was owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 personal pleasure flight, which was being conducted in the VFR traffic pattern, had been initiated less than five minutes prior to the accident. No flight plan had been filed, and there was no report of an ELT activation. According to the FAA Inspector who interviewed the pilot, while on downwind he thought that the aircraft was not responding to his lateral control inputs in the manner he expected it to. He therefore decided to continue around the pattern and make a full-stop landing. Because it seemed to the pilot that a reduction in engine power positively effected the perceived control problem, he reduced power on downwind and then attempted to turn base. Witnesses said that just prior to the base turn, the aircraft appeared to be going very slow. They also reported that as the aircraft entered a left bank, it appeared to fall out of the sky. Just prior to impacting the ground, the aircraft rolled back to a near wings-level position. According to the pilot/owner, no problem with the lateral flight control system was able to be identified, and no reason for the perceived lateral control anomaly was determined. After turning downwind in the experimental aircraft, the pilot sensed that the lateral flight controls were not responding to his inputs as he thought they would. He therefore elected to continue around the pattern and land. Because he felt that a reduction in power positively effected the perceived control problem, he reduced power on downwind and then attempted to turn base. Witnesses said that the aircraft was going very slow prior to turning base, and that as it entered a left bank, it fell out of the sky. Just prior to impacting the ground, the aircraft rolled wings-level. No problem with the lateral flight control system was able to be identified, and no reason for the perceived lateral control anomaly was determined. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_SEA98LA185.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 ↗