Casualties unknown

Nose Gear Collapse During MD-11F Landing (N250UP)

Louisville, KY, US

On June 7, 2005, a Mcdonnell Douglas MD-11F (registration N250UP) was involved in an aviation accident near Louisville, KY. Investigators recorded the probable cause as: The flying pilot's improper aircraft handling after main landing gear touchdown, which resulted in the collapse of the nose landing gear assembly. Conributing to the accident was the pilot-in-command's inadequate supervision during the landing. 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
Aircraft registered N250UP
Aircraft registered N250UP. Photo: Frank Kovalchek from Anchorage, Alaska, USA / CC BY 2.0, via Wikimedia Commons

An MD-11F on a night landing experienced nose gear collapse after main gear touchdown. FDR data showed abrupt forward control column movement and excessive vertical loads. Metallurgy indicated overstress without preexisting fractures.

Incident Overview

A McDonnell Douglas MD-11F cargo aircraft sustained a nose landing gear collapse during landing on an 8,579-foot-long concrete runway. The flight was conducted under night visual meteorological conditions. The captain occupying the left seat was the pilot flying and was receiving initial operating experience (IOE). A captain seated in the right seat acted as the pilot-in-command (PIC) of the flight.

Sequence of Events

After the main landing gear touched down, the nose gear subsequently contacted the runway and collapsed. The airplane sustained damage to and around the pressure bulkhead at fuselage station 625.

Flight Data Recorder Analysis

Data from the flight data recorder (FDR) revealed that following main gear touchdown, the control column was moved sharply forward, resulting in a change in pitch attitude from approximately 5 degrees nose-up to about 1 degree nose-down. This movement was accompanied by a reduction in vertical load factor to approximately 0.3 g. Upon nose wheel contact, the vertical load factor spiked to approximately 2.5 g, which is over twice the value typical for a landing. The load factor increment of 0.75 g was also noted as excessive.

Metallurgical Examination

Metallurgical examination of the remnants of the nose landing gear assembly indicated that the failure was consistent with overstress. No evidence of any preexisting fractures was observed in the components.

Damage Assessment

The primary damage was localized to the area around the pressure bulkhead at station 625, with the nose landing gear collapsing under the excessive loads.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20050627X00874. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.