NTSB CAROL · Event
Event SEA07TA174
Registry · N391M
FAA Aircraft Registry record.
Make / Model
CESSNA T206H
Year of manufacture
2025
Engine
LYCOMING TIO-540-AJ1A (310 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
20250917
ADS-B equipped
Yes — Mode-S A48793
Registrant of record
STATE OF MONTANA DEPT OF NATURAL RESOURCES
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The complete loss of engine power during an attempted go-around from a simulated engine-out landing. Factors include rough/uneven terrain and high vegetation where the pilot made an emergency forced landing.
Factual narrative
On June 20, 2007, about 0930 mountain daylight time, a Cessna 185C, N391M, experienced a gear collapse during an engine-out emergency landing near Kalispell, Montana. The airline transport pilot, who was the sole occupant, was not injured, but the airplane, which is owned and operated by the United States Department of Agriculture Forest Service, sustained substantial damage. The 14 CFR Part 91 public-use personal proficiency flight, which departed Kalispell City Airport about 25 minutes prior to the accident, was being operated in visual meteorological conditions. No flight plan had been filed. According to the Forest Service, the pilot was practicing a simulated engine-out approach to a 1,800 foot private grass airstrip, with the intention of executing a go-around once he reached 100 feet above ground level (agl). During the approach, the pilot maintained a manifold pressure of about 12 inches, so that the engine would still be producing a small amount of power, and the throttle would not be completely closed. When the airplane reached a height of about 100 feet above the ground, the pilot moved the throttle partially forward in order to execute a go-around, but the engine rpm did not increase. The pilot then pushed the throttle full forward, but the propeller continued to only windmill. By the time the pilot determined that the engine had lost all power, it was too late to put the airplane down on the grass strip. The pilot therefore elected to make an emergency landing in a field past the departure end of the grass strip. The field where the airplane touched down was rough and uneven, and covered with high vegetation. About 15 feet beyond where the main landing gear came in contact with the terrain, the structure inside the right main landing gear attachment box failed, and the right main landing gear leg collapsed. When the right main gear leg collapsed, the right wing came in contact with the terrain. During a post-accident inspection of the airplane and engine, no anomalies could be found that would have lead to a loss of power. After the inspection, the Continental Motors IO-0470-F engine was started and run without any malfunction detected. The pilot was practicing a simulated engine-out approach to an 1,800-foot-private grass airstrip, with the intention of executing a go-around once he reached 100 feet above ground level (agl). During the approach, the pilot maintained a manifold pressure of about 12 inches, so that the engine would still be producing a small amount of power, and the throttle would not be completely closed. When the airplane reached a height of about 100 feet above the ground, the pilot moved the throttle partially forward in order to execute a go-around, but the engine rpm did not increase. The pilot then pushed the throttle full forward, but the propeller continued to only windmill. By the time the pilot determined that the engine had lost all power, it was too late to put the airplane down on the grass strip. The pilot therefore elected to make an emergency landing in a field past the departure end of the grass strip. The field where the airplane touched down was rough and uneven, and covered with high vegetation. About 15 feet beyond where the main landing gear came in contact with the terrain, the structure inside the right main landing gear attachment box failed, and the right main landing gear leg collapsed. When the right main gear leg collapsed, the right wing came in contact with the terrain. During a post-accident inspection of the airplane and engine, no anomalies could be found that would have lead to a loss of power. After the inspection, the Continental Motors IO-0470-F engine was started and run without any malfunction detected. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_SEA07TA174.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 (icing, go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
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- arXiv 2025 · arXiv preprint
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- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
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