NTSB CAROL · Event
Event SEA96LA020
Aircraft involved
Probable cause & findings
A LOSS OF ENGINE POWER DUE TO A CRACKED CYLINDER HEAD. A FACTOR WAS THE EVASIVE MANEUVER TO AVOID A DITCH.
Factual narrative
On November 15, 1995, at 1610 Pacific standard time, a Snow S2C, N1694S, experienced a loss of engine power during an aerial application flight. The pilot initiated a forced landing to an open field. During the landing roll, the airplane collided with rough terrain near Dufer, Oregon. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The airplane was substantially damaged and the commercial pilot, the sole occupant, was not injured. The flight had originated from Culver, Oregon, on November 15, 1995, at 1555. The pilot reported during an interview and subsequent written statement, that he was spraying a weed killer over a field at approximately ten feet above ground level, when the engine began to run rough and backfire. The airplane was unable to maintain altitude and the pilot initiated a forced landing to a field that was straight ahead and uphill. Prior to touch down, the pilot noticed a ditch and pulled up. The airplane stalled then landed hard. A post-crash inspection of the engine revealed a crack on the number five cylinder head. The crack travelled from the front to the rear spark plug hole. The pilot/owner reported that the engine had accumulated 950 hours since the last overhaul. Total time on the engine is unknown and a history on the cylinder is unknown. THE PILOT REPORTED THAT DURING AN AERIAL APPLICATION SPRAY RUN, THE ENGINE BEGAN TO RUN ROUGH AND BACKFIRE. THE AIRPLANE WAS UNABLE TO MAINTAIN ALTITUDE AND THE PILOT MADE A FORCED LANDING TO AN OPEN FIELD. PRIOR TO TOUCHDOWN, THE PILOT PULLED THE AIRPLANE UP TO MISS A DITCH. THE AIRPLANE STALLED AND THEN LANDED HARD. POSTCRASH INSPECTION OF THE ENGINE REVEALED A CRACK IN THE HEAD ON THE #5 CYLINDER. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_SEA96LA020.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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