Casualties unknown

2002-03-22: Mcdonnell Douglas DC-10-30 (N234NW) — Northwest Airlines — Int'l Waters

Int'l Waters, US

On March 22, 2002, a Mcdonnell Douglas DC-10-30 (registration N234NW) operated by Northwest Airlines was involved in an aviation accident near Int'l Waters. Investigators recorded the probable cause as: The main pitchover, which likely caused the flight attendant's injuries, occurred as a result of control column inputs made by the first officer. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 6 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards
Aircraft registered N234NW
Aircraft registered N234NW. Photo: Cory W. Watts from Madison, Wisconsin, United States of America / CC BY-SA 2.0, via Wikimedia Commons

A flight attendant was seriously injured during turbulence while the aircraft descended from FL350 to FL340. The flight crew did not brief the lead flight attendant on turbulence level or duration, and the lead flight attendant did not relay the information. The pitchover that caused the injury resulted from the first officer's control inputs.

Incident Summary

A flight attendant sustained serious injuries when the aircraft encountered turbulence during a descent from flight level (FL) 350 to FL 340. The flight crew stated in interviews that they were preparing for turbulence and wanted passengers and flight attendants seated with seatbelts fastened.

Flight Crew Actions

According to the investigation, the flight crew did not advise the lead flight attendant (LFA) of the turbulence level or its anticipated duration, nor did they use turbulence codes as required by Northwest Airlines' Flight Operations Manual. Additionally, the LFA did not relay turbulence information to all flight attendants, as stipulated in the company's Flight Attendant Manual.

Restraint System Examination

Examination of the restraint system from the injured flight attendant's jump seat revealed that the system did not fail during the turbulence upset. Investigators were unable to determine whether the lapbelt was improperly secured by the flight attendant or inadvertently disengaged during the event.

Flight Data Analysis

Analysis of flight data recorder (FDR) data indicated that the turbulence caused substantial vertical and lateral oscillations, which may have made it difficult for the first officer, who was the flying pilot, to maintain a constant pitch attitude. The FDR showed variations in pitch attitude during the turbulence encounter. Flight crew statements indicated they were attempting to maintain constant pitch attitudes, but FDR data showed that large and rapid pitch excursions were primarily the result of control column inputs made by the first officer.

Determination

The Safety Board's investigation determined that the main pitchover, which likely caused the flight attendant's injuries, occurred as a result of the first officer's control inputs.

Probable cause

The main pitchover, which likely caused the flight attendant's injuries, occurred as a result of control column inputs made by the first officer.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020322X00387. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.