Uncommanded roll and vibration in Airbus A320

Casualties unknown • Chattanooga, TN, US

During a climb following takeoff, an aircraft experienced intense vibrations and an uncommanded right roll, leading to an emergency landing.

What happened

Shortly after takeoff, the flight crew of the Airbus A320 experienced a high-frequency vibration that was perceptible through the control column and at the crew's feet. Although the engine indicating and alerting system displayed no messages, the slow-frequency vibration increased in intensity over approximately 30 seconds.

As the aircraft climbed toward its cleared altitude of 17,000 feet, it began an uncommanded roll to the right. The first officer disconnected the autopilot to regain manual control of the aircraft. Following the event, the captain declared an emergency, and the crew was cleared to proceed to an alternate airport. The vibrations persisted throughout the descent and continued during the landing phase.

The investigation

Mechanical examination of the aircraft focused on the aileron system. Investigators discovered that the bushings and the inboard and outboard power control unit output links for the right aileron were worn. This wear exceeded the tolerances permitted by the maintenance manual. Additionally, it was noted that the manufacturer's inspection procedures for checking aileron system backlash did not require the operator to record the specific tolerances found during the check.

Probable cause

Excessive wear of the right aileron bushings and power control unit output links beyond allowable limits.

Frequently asked questions

What happened in the 2003-05-08 Canadair CL-600-2B19 accident near Chattanooga, TN?

During a climb following takeoff, an aircraft experienced intense vibrations and an uncommanded right roll, leading to an emergency landing.

What aircraft was involved and where did it happen?

The accident on 2003-05-08 involved a Canadair CL-600-2B19, registration N829AS, operated by Atlantic Southeast Airlines, Inc., at Chattanooga, TN.

What was the probable cause of the accident?

Excessive wear of the right aileron bushings and power control unit output links beyond allowable limits.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030516X00677. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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