Casualties unknown

Engine Failure Prompts Forced Landing and Fence Collisions (N7113K)

Clear Lake, MN, US

On January 20, 2002, a Piper PA-18 (registration N7113K) was involved in an aviation accident near Clear Lake, MN. Investigators recorded the probable cause as: The loss of engine power for undetermined reasons and the unsuitable terrain for the forced landing. Factors were the low altitude and the fences. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A pilot conducted a forced landing after engine failure at 400 feet, hitting two fences. Post-accident examination found no anomalies. Temperature and dewpoint data suggested light carburetor icing conditions.

Accident Overview

A single-engine airplane experienced an engine failure while in the traffic pattern and subsequently collided with two fences during a forced landing to a field. The pilot, who had performed three run-ups and intended to conduct take-offs and landings following an annual inspection, reported that the engine lost power and quit at approximately 400 feet above ground level. At the time, the pilot had just turned from the crosswind leg to the downwind leg of the traffic pattern.

Pilot Actions

The pilot stated that he could not return to the airport due to insufficient altitude and could not land directly ahead because of obstructions. He attempted to land in a field, but the field lacked adequate space, resulting in the airplane striking two fences before coming to rest.

Post-Accident Examination

A detailed examination of the airplane after the accident 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, indicating no mechanical malfunction was evident.

Weather Conditions

The weather observing station, located approximately 7 miles and 330 degrees from the accident site, recorded a temperature of -3 degrees Celsius and a dewpoint of -7 degrees Celsius at 1453. According to a Transport Canada carburetor icing probability chart, these temperature and dewpoint values fall within the range for light icing at cruise or descent power.

Conclusion

The source provides no stated cause for the accident.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020129X00148. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.