Casualties unknown

Engine Failure on ValuJet Flight 224 Prompts Emergency Landing (N930VV)

Dfw Airport, TX, US

On December 12, 1995, a Mcdonnell Douglas DC-9-32 (registration N930VV) was involved in an aviation accident near Dfw Airport, TX. Investigators recorded the probable cause as: Failure of a first stage high pressure turbine blade due to fatigue. 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

After takeoff, the No. 2 engine of a ValuJet DC-9-32 suffered a contained failure due to a turbine blade fatigue failure. The crew secured the engine and landed safely on one engine.

Incident Overview

On an unspecified date, ValuJet Flight 224, a McDonnell Douglas DC-9-32 (registration not provided), experienced a failure of the No. 2 engine during the climb. The aircraft had just departed and was climbing through approximately 5,000 feet when the engine failure occurred. The crew promptly secured the affected engine and declared an emergency. Air traffic control vectored the aircraft back to the departure airport, where a single-engine landing was completed without further incident.

Engine Examination

Post-incident examination and teardown of the Pratt & Whitney JT8D-9A engine revealed that a turbine blade (part number 823201) in the first stage high pressure turbine assembly had failed due to fatigue. The blade's part number indicated that its leading edge had been reworked in accordance with Pratt & Whitney Service Bulletin 4345 to address cracking. The engine had accumulated a total of 32,028 flight hours and 25,603 cycles since new, and 2,794 flight hours and 2,329 cycles since its last overhaul.

Conclusions

No other anomalies were found during the investigation. The failure was contained within the engine, and no further damage to the aircraft was reported. No injuries were mentioned in the source material.

Probable cause

Failure of a first stage high pressure turbine blade due to fatigue.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X04999. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.