Casualties unknown

Multi-Engine Airplane Strikes Obstacles After Power Loss During Initial Climb (N63887)

Detroit, MI, US

On November 8, 2004, a Piper PA-23-250 (registration N63887) operated by Willie L. Shaw was involved in an aviation accident near Detroit, MI. Investigators recorded the probable cause as: The pilot's failure to feather the propeller and to maintain control of the airplane following the loss of engine power which resulted from undetermined reasons. 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 multi-engine airplane lost power on one engine shortly after takeoff, leading to a collision with power lines, a house, a tree, and a fence. The left engine propeller was not feathered. Post-accident inspection found no mechanical failure.

Accident Summary

A multi-engine airplane experienced a loss of engine power during the initial climb after takeoff, resulting in a collision with power lines, a house, a tree, and a fence. A second house sustained fire and impact damage from flying debris. The pilot reported that all engine indications were normal until after takeoff.

Events

According to the pilot, he noticed a "split" in manifold pressure and rpm at approximately 50 feet above ground level, indicating a loss of power on the left engine. He turned to the south (left) to avoid obstacles and attempted to land in a field. A pilot-rated passenger reported that after takeoff, the pilot "seemed to be having problems gaining and maintaining altitude." She stated that she thought the pilot was returning to the airport when they began to lose altitude, and that she heard the stall warning horn come on twice during the flight. She was busy making call-outs and looking at airspeed, and therefore did not know which engine had lost power or if the propeller had been feathered.

Inspection Findings

Both engines sustained heat and impact damage. Post-accident inspection of the engines failed to reveal any failure or malfunction that would have resulted in the loss of engine power. Detailed inspection of the left engine propeller revealed that the propeller had not been feathered prior to impact. The airplane information manual states that once the faulty engine is identified and its power loss verified, its propeller should be feathered.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20041112X01809. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.