Casualties unknown

Uncontained Engine Failure Forces Rejected Takeoff and Evacuation of ValuJet Flight 597 (N908VJ)

Atlanta, GA, US

On June 8, 1995, a Douglas DC-9-32 (registration N908VJ) was involved in an aviation accident near Atlanta, GA. Investigators recorded the probable cause as: The uncontained failure of the right engine due to fatigue failure of its 7th stage high compressor disc, which originated at a stress redistribution hole and was not detected during overhaul due to inadequate recordkeeping and failure to use process sheets… This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 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

During takeoff roll, ValuJet Flight 597 experienced an uncontained right engine failure, leading to a cabin fire and evacuation. One flight attendant suffered serious injuries; six others minor injuries. Fatigue failure of a compressor disc was identified as the cause.

Incident Overview

On an unspecified date, ValuJet Flight 597 began its takeoff roll when occupants heard a loud bang. The right engine fire warning light illuminated, and the crew of a following aircraft reported that the right engine was on fire. The takeoff was rejected. Shrapnel from the right engine penetrated the fuselage and the right engine main fuel line, causing a cabin fire to erupt. The airplane was brought to a stop on the runway, and the captain ordered an evacuation.

Injuries and Damage

One flight attendant sustained serious puncture wounds from shrapnel and thermal injuries. Another flight attendant and five passengers received minor injuries. The aircraft sustained damage from shrapnel penetration and fire.

Investigation Findings

The investigation determined that an uncontained failure of the right engine occurred due to fatigue failure of its 7th stage high compressor disc. The fatigue crack originated at a stress redistribution hole in the disc. Analysis of fatigue striation measurements indicated that the crack had developed before the disc was last overhauled at a repair station (Turk Hava Yollari) in 1991, but was not detected during that overhaul.

Repair Station Issues

Further investigation of the repair station revealed evidence of inadequate recordkeeping and a failure to use 'process sheets' to document step-by-step overhaul and inspection procedures. These deficiencies were noted as contributing factors to the undetected fatigue crack.

Reference

Additional information can be found in NTSB/AAR-96/03.

Probable cause

The uncontained failure of the right engine due to fatigue failure of its 7th stage high compressor disc, which originated at a stress redistribution hole and was not detected during overhaul due to inadequate recordkeeping and failure to use process sheets by the repair station (Turk Hava Yollari).

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X03623. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.