NTSB CAROL · Event
Event WPR17LA191
Registry · N8695H
FAA Aircraft Registry record.
Make / Model
NORTH AMERICAN NAVION A
Engine
CONT MOTOR E225 SERIES (225 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
19551230
ADS-B equipped
Yes — Mode-S ABF355
Registrant of record
MOAK ERIC DAVID
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A total loss of engine power for reasons that could not be determined because postaccident examination of the engine revealed no evidence of any preaccident mechanical malfunctions or failures that would have that would have precluded normal operation.
Factual narrative
On August 27, 2017, about 1620 Pacific daylight time, a North American Navion A airplane, N8695H, experienced a total loss of engine power during the initial climb from Rohnerville Airport, Fortuna, California. The private pilot was not injured; the airplane sustained substantial damage to the firewall during the forced landing. The airplane was registered to and operated by the pilot as a Title 14 Code of Federal Regulations Part 91 personal flight. Visual meteorological conditions prevailed and no flight plan had been filed for the local flight which departed from Fortuna about 1615. The pilot stated that he departed with about 10-12 gallons of fuel on board. After the airplane reached about 1,000 ft above ground level (agl), the engine experienced a total loss of power. He attempted to return back to the airport, but was unable to maintain altitude and he made an off-airport landing in a pasture about .5 miles from the runway at Fortuna. A Federal Aviation Administration (FAA) certificated airframe and powerplant mechanic completed a post accident examination under the auspice of an FAA inspector. The inspector noted that the original engine for this airplane was replaced by a Teledyne Continental Motors IO-470H which was installed in June 2003. The spark plugs were removed from all cylinders revealing no signs of deterioration, wear or oil/carbon fouling. Continuity was established for each magneto, which produced spark at each cylinder. A borescope inspection of each cylinder revealed no evidence of excessive wear, deterioration, broken rings, or broken valves. The FAA inspector further stated that he observed fuel in the left, right, and main tanks. He sumped samples from each tank disclosing that there was no debris or water visible. Disassembly of the fuel manifold revealed a clean screen; there was no fuel visible. The mechanic removed the fuel inlet supply line to the fuel manifold and activated the electric fuel boost pump. Fuel flowed normally out of the inlet supply line from the tank that was selected, all of which were selected. The reason for the loss of power was not determined. The private pilot stated that, after departing for the local, personal flight and as the airplane reached about 1,000 ft above ground level, the engine lost all power. He attempted to return to the airport, but the airplane was unable to maintain altitude, so he chose to make an off-airport landing in a pasture, during which the firewall sustained substantial damage. Postaccident examination of the engine revealed no evidence of any preaccident mechanical malfunctions or failures that would have precluded normal operation. The reason for the loss of engine power could not be determined. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2017_WPR17LA191.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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