Casualties unknown

MD-82 Takeoff Incident Involves Flight Control Malfunction (N934AS)

Fairbanks, AK, US

On February 5, 1999, a Mcdonnell Douglas MD-82 (registration N934AS) operated by Alaska Air Group, Inc was involved in an aviation accident near Fairbanks, AK. Investigators recorded the probable cause as: The restricted/delayed movement of the elevator flight control due to extremely cold weather conditions. 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 N934AS
Aircraft registered N934AS. Photo: Aeroprints.com / CC BY-SA 3.0, via Wikimedia Commons

A McDonnell Douglas MD-82 crew reported a partial flight control malfunction during takeoff, with the nose failing to rise until excessive yoke pressure was applied. Post-flight inspection found no anomalies, and FDR data showed elevators initially down.

Incident Report

The crew of a McDonnell Douglas MD-82 airplane reported a partial flight control malfunction during takeoff. The captain stated that during the takeoff roll, the airplane's nose failed to rise as he applied aft control yoke pressure. When he applied an excessive amount of aft control yoke pressure, the nose rotated slowly, and the airplane assumed the desired pitch angle for takeoff. Prior to the incident flight, the incident airplane remained parked outside overnight. During the night, the air temperature dropped below minus 50 degrees Fahrenheit.

Inspection and Findings

Following the incident, the airplane underwent an extensive inspection and evaluation of the flight control system. Company maintenance personnel discovered no flight control anomalies during this process.

Flight Data Recorder Analysis

The NTSB's flight data recorder (FDR) readout showed that during the initial phase of the incident takeoff roll, both elevators remained in a down position. As the takeoff roll progressed and the airspeed approached 150 knots, both elevators responded to the pilot's control column inputs, and the nose of the airplane rotated. The pilot's control column position was not a recorded parameter of the incident airplane's FDR.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001205X00119. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.