Left wing separation following engine fire during return to airport

Casualties unknown • Newville, AL, US

An aircraft experienced a left wing separation and subsequent crash after the pilot reported power loss in the left engine during a return to the airport.

What happened

Following maintenance performed on the engine turbochargers and exhaust systems several days prior to the flight, the pilot departed and subsequently reported that the left engine lost power. In response to the power loss, the pilot elected to return to the airport.

A witness observed the aircraft heading toward the airport with an orange glow visible under the left wing, approximately four feet outboard of the fuselage. The witness then heard a loud pop, after which the left wing separated from the airplane, causing the aircraft to fall to the ground.

The investigation

Post-accident inspection revealed extensive fire damage located in the area of the left wheel well and spar. This damage was situated behind the firewall, immediately aft of the turbocharger exhaust. During the examination, it was found that fuel lines in the wheel well area had burned away. Additionally, the left engine turbocharger tail pipe and the Marmon connector clamp were missing from the aircraft. The engines involved were equipped with AiResearch turbochargers under STC SA909WE.

Probable cause

The loss of power in the left engine and subsequent wing separation was caused by fire damage to the left wheel well and spar, following the failure or absence of the turbocharger tail pipe and connector clamp.

Frequently asked questions

What happened in the 1994-10-23 Piper PA-23-250 accident near Newville, AL?

An aircraft experienced a left wing separation and subsequent crash after the pilot reported power loss in the left engine during a return to the airport.

What aircraft was involved and where did it happen?

The accident on 1994-10-23 involved a Piper PA-23-250, registration N999BW, operated by Mann, Nathaniel E., at Newville, AL.

What was the probable cause of the accident?

The loss of power in the left engine and subsequent wing separation was caused by fire damage to the left wheel well and spar, following the failure or absence of the turbocharger tail pipe and connector clamp.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X02374. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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