Casualties unknown

Pilot Fatally Injured in Crash After Loss of Power on Takeoff (N1069P)

Dodge Center, MN, US

On July 22, 2000, a Piper PA-23 (registration N1069P) was involved in an aviation accident near Dodge Center, MN. Investigators recorded the probable cause as: The pilot not maintaining airplane control in his turn back in the direction of the airport and the pilot not performing an emergency landing straight ahead. 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

An airplane was destroyed during a terrain impact and post-accident fire following a loss of power on takeoff. The pilot sustained fatal injuries. Investigation revealed water and debris in the fuel system, including partially blocked carburetor screens.

Accident Narrative

The airplane was destroyed when it impacted terrain and was subsequently consumed by a post-accident fire. The accident occurred during a maneuver to return to the airport after experiencing a loss of power on takeoff. The pilot was fatally injured. The annual inspection had been completed on July 21, 2000.

Witness Observations

A witness reported that the airplane was just above power lines before it made a turn to the east. The airplane then turned back to the north at a lower altitude. According to the witness, the airplane impacted the ground with its left wing first, followed by the nose. After impact, the airplane spun around and burst into flames. The witness stated that the engine was sputtering prior to the crash. The witness called 911 at 1440.

Fuel and Engine Information

A fuel pump log indicated the airplane was last fueled at 1429. Continuity to all control surfaces and to both engines was established. A thumb compression was found at all cylinders. All magnetos, except the right engine's left magneto, produced spark when rotated.

Fuel System Examination

A liquid was found in the left engine's carburetor bowl. Analysis of the liquid revealed the presence of water and a flammable liquid consistent with aviation fluid. Additionally, the liquid contained mineral matter, plant matter, fibers, glass-like particles, metallic particles, and unidentified particles.

Both carburetor inlet screens contained a media. The NTSB Materials Laboratory report stated that examination of the cylindrical screen revealed the sides were partially blocked with debris and the round end was totally blocked. Approximately 60% of the right screen mesh was blocked with debris, and approximately 30% of the left screen mesh was blocked.

Propeller and Governor Examination

Both propellers exhibited witness marks indicating low blade angle, and no anomalies were found. The left governor was tested and had no anomalies found. The right governor was not tested.

Emergency Landing Considerations

Review of aerial photographs showed that there were suitable fields for emergency landings around the airport.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X21371. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.