Casualties unknown

Horizontal Stabilizer Trim Failure Due to Improper Overhaul on DC-10-30 (N270AX)

Atlanta, GA, US

On May 2, 2007, a Mcdonnell Douglas DC-10-30 (registration N270AX) operated by Omni Air International Inc was involved in an aviation accident near Atlanta, GA. Investigators recorded the probable cause as: Improper overhaul of the horizontal stabilizer chain drive unit drive assembly by omission of one pin, one nut, and one washer, which caused fatigue failure of another pin and shear failure of the installed pin, preventing transmission of drive assembly… 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 N270AX
Aircraft registered N270AX. Photo: Christopher Kern ( Albion ) / CC BY 3.0, via Wikimedia Commons

A DC-10-30 experienced inability to move the horizontal stabilizer during flight due to improper overhaul of the drive assembly, missing securing parts. The crew declared an emergency and landed uneventfully.

Incident Overview

During a flight at 13,000 feet mean sea level (msl), while decelerating to 250 knots, the horizontal stabilizer on a DC-10-30 airplane could not be moved by either autopilot commands or the primary and alternate control switches in the cockpit. The stabilizer remained at approximately 1 degree airplane nose-up, resulting in excessive cockpit control forces. The flight crew declared an emergency with air traffic control and subsequently landed without further incident on runway 27R at Hartsfield-Jackson Atlanta International Airport (ATL).

Maintenance History

The horizontal stabilizer drive assembly, part number AJH 7337-507 and serial number DCA-418, had been overhauled on April 30, 1999. It was installed in the incident airplane on April 23, 2006. At the time of the incident, the airplane had accumulated 2,421 hours and 473 cycles since installation of the overhauled assembly. Review of flight crew write-ups found no entries related to pitch trim for the preceding 93 days.

Cause of Failure

Investigation determined that the inoperative horizontal stabilizer trim system was caused by improper overhaul of the horizontal stabilizer chain drive unit drive assembly. During the overhaul, one pin (part number 3D0009-5-4), one nut (part number MS21043-08), and one washer (part number NAS 1252-BL) were omitted. These parts were necessary to secure the drive gear of the horizontal stabilizer drive assembly. The omission led to fatigue failure of another pin (part number AJH7378-1) and shear failure of the single installed pin (part number 3D0009-5-4). As a result, the output of the horizontal stabilizer drive assembly could not be transmitted to the acme screws of the horizontal stabilizer, rendering the trim system inoperable.

Probable cause

Improper overhaul of the horizontal stabilizer chain drive unit drive assembly by omission of one pin, one nut, and one washer, which caused fatigue failure of another pin and shear failure of the installed pin, preventing transmission of drive assembly output to the acme screws.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20070510X00542. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.