Casualties unknown

Engine Malfunction Prompts Takeoff Abort and Evacuation (N3507A)

Dfw Airport, TX, US

On November 23, 1996, a Mcdonnell Douglas MD-82 (registration N3507A) operated by American Airlines was involved in an aviation accident near Dfw Airport, TX. Investigators recorded the probable cause as: The failure of the low pressure turbine shaft. A factor was the coke build up on the low pressure turbine shaft. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards
Aircraft registered N3507A
Aircraft registered N3507A. Photo: Bill Abbott / CC BY-SA 2.0, via Wikimedia Commons

During takeoff, a thump and left nose pull led to an aborted departure. Crews reported left engine fire; captain ordered evacuation. Fire was confined to tailpipe; turbine blades from the number 4 disk penetrated the case, damaging pylon and empennage.

Incident Overview

The aircraft was departing when the pilots felt a thump accompanied by a slight left nose pull, prompting them to abort the takeoff. After taxiing clear of the runway and coming to a stop, several flight crews on the ground reported over the tower frequency that the incident airplane's left engine was on fire. The captain initiated an evacuation of the airplane.

Firefighting Response

Airport Rescue and Fire Fighting (ARFF) personnel reported that the engine fire was confined to the tailpipe area. No further spread of fire was noted.

Engine Damage

Turbine blades had separated from the number 4 turbine disk, penetrated the engine case, and subsequently damaged the engine pylon and empennage area.

Teardown Examination

A teardown examination of the engine revealed that the Low Pressure Turbine (LPT) shaft was deformed and fractured into two pieces. Heavy coke deposits were identified on both the outer diameter of the LPT shaft and the inner diameter of the center tube. The two pieces of the LPT shaft were twisted and subjected to considerable permanent deformation, with the amount of plastic deformation indicative of exposure to high temperatures. Additionally, the High Pressure Turbine shaft was found with a missing 4 1/2 bearing stack retention pin, one of three such pins.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X07025. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.