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Atlas / NTSB / SEA07TA174

NTSB CAROL · Event

Event SEA07TA174

2007-06-20 Kalispell, Montana, United States None 1 aircraft Status: Completed

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 ↗.

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.

Browse the full corpus — academia portal ↗