NTSB CAROL · Event
Event SEA97LA122
Registry · N1923S
FAA Aircraft Registry record.
Make / Model
RENQUIST JOHN H STARDUSTER TOO SA300
Year of manufacture
1984 · 13 years old at event
Engine
LYCOMING I0360 SER A&C (200 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19981021
ADS-B equipped
Yes — Mode-S A1726B
Registrant of record
KIM STEVEN S
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain directional control of the airplane. Related factors include: an area of standing water on a portion of the runway, and soft terrain just off the edge of the runway.
Factual narrative
On May 27, 1997, approximately 1030 mountain daylight time, a Noe SA-300 experimental biplane, N1923S, nosed over after departing the side of the runway at Bountiful Skypark, Bountiful, Utah. The private pilot, who was the sole occupant, was not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 local personal pleasure flight had been in the air about 30 minutes at the time of the accident. No flight plan had been filed, and the flight was being conducted in visual meteorological conditions. According to the pilot, he executed a full-stall landing, and during the landing roll, the aircraft moved to the right side of the runway where its right main gear hit a pool of water on the runway surface. This pulled the aircraft further to the right, and the pilot was unable to keep it from departing the right side of the runway. After departing the runway, the aircraft entered an area of soft dirt and flipped over. A review of the pilot's log revealed that he had been receiving dual instruction in the aircraft for about 60 days prior to the accident. During that period of time, he had logged over 220 landings, and had received his conventional gear/ tailwheel endorsement after a flight that had occurred earlier on the day of the accident. The pilot was on his first solo flight after receiving his tailwheel/conventional endorsement earlier on the same day. During the landing roll, he allowed his experimental biplane to move toward the right side of the runway, where its right main gear encountered standing water. The aircraft was pulled further to the right by the resistance of the right main tire passing through the water, and the aircraft ultimately exited the right side of the runway. After departing the runway, the aircraft entered an area of soft terrain, resulting in a nose-over. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_SEA97LA122.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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