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CHI02LA065

2002-01-20 · Clear Lake, Minnesota, United States · None · 1 aircraft · Status: Completed

Airport 8Y6

Current FAA registration · N7113K

Make / Model
PIPER PA-18
Year of manufacture
1950 · 52 years old at event
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19700630
ADS-B equipped
Yes — Mode-S A9828F

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The loss of engine power for undetermined reasons and the unsuitable terrain for the forced landing. Factors were the low altitude and the fences.

Factual narrative

On January 20, 2002, about 1500 central standard time, a Piper PA-18, N7113K, owned and piloted by a private pilot, sustained substantial damage when it collided with fences during a forced landing to a field near Clear Lake, Minnesota. The airplane was reported to have lost engine power during climb out after takeoff from runway 18 (3,000 feet by 150 feet, asphalt/turf), at the Leaders Clear Lake Airport, Clear Lake, Minnesota. The 14 CFR Part 91 personal flight was not on a flight plan and was operating in visual meteorological conditions. The local flight was originating at the time of the accident. In a written statement, the pilot said that he had performed three "run ups" and was going to perform "...some take-offs and landings after the annual." He said that after take-off, at about 400 feet agl, the engine lost power and quit. He said that he had just turned from the crosswind leg of the traffic pattern to the downwind leg. The pilot stated that he could not make it back to the airport, and could not land directly ahead due to obstructions. The pilot said that he attempted to land in a field but the field did not have enough room for the landing and he hit two fences before coming to rest. A postaccident examination of the airplane revealed no anomalies that could be associated with a pre-impact condition. The engine was subsequently test run on the airframe and no anomalies were found. The weather observing station located about 7 miles and 330 degrees from the accident recorded the temperature as -3 degrees Celsius and the dewpoint as -7 degrees Celsius at 1453. According to a Transport Canada carburetor icing probability chart, the temperature and dew point fall in the range for light icing at cruise or descent power. The airplane collided with two fences during a forced landing to a field following an engine failure while in the traffic pattern. The pilot said that he had performed three "run ups" and was going to perform "...some take-offs and landings after the annual." He said that after take-off, at about 400 feet agl, the engine lost power and quit. He said that he had just turned from the crosswind leg of the traffic pattern to the downwind leg. The pilot stated that he could not make it back to the airport, and could not land directly ahead due to obstructions. The pilot said that he attempted to land in a field but the field did not have enough room for the landing and he hit two fences before coming to rest. A postaccident examination of the airplane revealed no anomalies that could be associated with a pre-impact condition. The engine was subsequently test run on the airframe and no anomalies were found. The weather observing station located about 7 miles and 330 degrees from the accident recorded the temperature as -3 degrees Celsius and the dewpoint as -7 degrees Celsius at 1453. According to a Transport Canada carburetor icing probability chart, the temperature and dewpoint fall in the range for light icing at cruise or descent power. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2002_CHI02LA065.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

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