Single-Engine Power Loss During Initial Climb Leads to Fatal Crash

Casualties unknown • Chico, CA, US

A pilot died following an engine failure during the initial climb phase, resulting in a wing-low descent and subsequent aircraft fire.

What happened

During the initial climb following takeoff, witnesses observed the airplane reach a maximum altitude of 200 feet above the runway. The aircraft then entered a right wing low attitude and descended into level ground, striking the area short of the airport's perimeter fence. Upon impact, a fire erupted that consumed the entire aircraft.

The pilot sustained fatal injuries. Before passing away, the pilot informed medical personnel that the engine had failed while he was attempting to execute a turn.

The investigation

An examination of the airframe revealed fire damage to the wings in areas corresponding to both the inboard and outboard fuel tanks. The fuel selectors were found in the main tank positions, and the landing gear was extended at the time of the accident. The rudder trim tab was set to a position consistent with a power failure on the right engine.

Mechanical inspection of the engines showed no evidence of internal mechanical malfunction. While the left propeller blades exhibited torsional twisting and gouging, the right propeller blades sustained only minor damage.

The pilot, who was an airframe and powerplant mechanic, had performed recent maintenance on the aircraft himself. This flight was the first since that maintenance, which occurred approximately 3.5 months prior. Investigators found no logbook records identifying the specific maintenance performed. Based on the aircraft weight and prevailing meteorological conditions, performance data indicated the airplane should have maintained a positive climb rate if the right engine's propeller had been feathered and the landing gear retracted.

Findings

Investigators were unable to determine the cause of the nonmechanical loss of power in the right engine.

Probable cause

The cause of the right engine's nonmechanical loss of power could not be determined.

Frequently asked questions

What happened in the 2001-09-10 Piper PA-23-150 accident near Chico, CA?

A pilot died following an engine failure during the initial climb phase, resulting in a wing-low descent and subsequent aircraft fire.

What aircraft was involved and where did it happen?

The accident on 2001-09-10 involved a Piper PA-23-150, registration N2268P, at Chico, CA.

What was the probable cause of the accident?

The cause of the right engine's nonmechanical loss of power could not be determined.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010920X01974. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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