Aircraft overruns runway during aborted takeoff

Casualties unknown • Tecumseh, MI, US

An aircraft failed to rotate during an aborted takeoff, resulting in a runway overrun and significant structural damage after colliding with soft terrain.

What happened

During an aborted takeoff, the aircraft overran the runway and collided with soft terrain. The pilot reported that the preflight, engine start, and engine run-up procedures were all completed normally.

As the aircraft reached 85 knots, the pilot attempted to rotate by pulling back on the yoke. The control movement was minimal, and the airplane failed to rotate despite a second, harder application of the yoke. In response, the pilot cut the throttle and applied full brakes. The aircraft subsequently traveled off the end of the runway, crossed a road, and entered a plowed field. The impact with the soft terrain caused the nose gear to collapse and resulted in both main gears separating from the airplane.

The investigation

An inspection of the flight control systems revealed no failures or malfunctions. However, an examination of the engine identified that the three screws securing the magneto harness cover on the right magneto were missing, which had allowed the harness to back away from the magneto. Additionally, investigators found that the turbine in the turbocharger was dragging during a manual rotation attempt. A teardown of the turbocharger subsequently revealed a build-up of carbon within the heat shield.

Probable cause

The investigation identified missing screws on the right magneto harness cover and carbon build-up in the turbocharger heat shield, though no flight control failure was found.

Frequently asked questions

What happened in the 2000-10-15 Piper PA-32R-301T accident near Tecumseh, MI?

An aircraft failed to rotate during an aborted takeoff, resulting in a runway overrun and significant structural damage after colliding with soft terrain.

What aircraft was involved and where did it happen?

The accident on 2000-10-15 involved a Piper PA-32R-301T, registration N289JG, operated by James A. Gecsei, at Tecumseh, MI.

What was the probable cause of the accident?

The investigation identified missing screws on the right magneto harness cover and carbon build-up in the turbocharger heat shield, though no flight control failure was found.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22122. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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