Casualties unknown

Left Engine Failure and Emergency Descent to Whiteman Air Force Base (N9413T)

Whiteman Afb, MO, US

On July 12, 2001, a Mcdonnell Douglas MD-83 (registration N9413T) operated by Trans World Airlines, Llc was involved in an aviation accident near Whiteman Afb, MO. Investigators recorded the probable cause as: The separation of a fan blade due to fatigue failure which led to case separation and loss of engine power in the left engine. 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

An MD-83 experienced left engine failure at 31,000 feet due to a fatigue-fractured fan blade. The crew received an incorrect ILS frequency, descended below minimum vectoring altitude, and performed a radar approach to Whiteman AFB.

Engine Failure and Emergency Descent

The McDonnell Douglas MD-83, operating as a scheduled passenger flight, experienced a catastrophic failure of the left engine while at 31,000 feet. The flightcrew heard a thud and observed the left engine surging. White smoke filled the cabin and cockpit, prompting the crew to don oxygen masks, declare an emergency, and initiate an emergency descent to Kansas City International Airport (MCI), Kansas City, Missouri.

Diversion to Whiteman Air Force Base

During the descent toward MCI, the crew changed their landing destination to Whiteman Air Force Base (SZL), Knob Noster, Missouri, when approximately 18 miles north of SZL. The airline did not provide approach charts for SZL to its flight crews. The flight crew requested the ILS frequency for runway 19 from air traffic control (ATC) and received an incorrect frequency. They also requested and were given the inbound course for ILS 19 but never obtained the correct ILS frequency for the remainder of the flight, relying instead on a radar approach to SZL.

Descent Below Minimum Vectoring Altitude

During the radar approach, ATC instructed the flightcrew to maintain a minimum vectoring altitude of 2,500 feet mean sea level. The crew descended below this altitude to 1,800 feet msl in order to descend below a cloud layer that was at 1,400 feet above ground level.

Examination of the Engine

Metallurgical examination revealed a fatigue fracture of one fan blade. Examination of the left engine showed that the fan exit case had a 360-degree fracture. Several service bulletins (SBs) applicable to the fan exit case introduced a newer steel engine case to replace the older aluminum case and recommended installation of stops to restrict axial separation of the case in the event of fracturing. The SBs noted that there had been five instances of full 360-degree fan exit case fracture, all due to fan blade fracture, and that when the case fractures, the front of the engine with the cowl shifts forward. The incident engine had an aluminum fan exit case and did not have stops installed.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010717X01445. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.