Casualties unknown

Uncommanded Rolls Prompt Inspection of Sidestick Transducer Unit on A320 (N331NW)

Minneapolis, MN, US

On April 28, 1995, an Airbus Industrie A320-211 (registration N331NW) was involved in an aviation accident near Minneapolis, MN. Investigators recorded the probable cause as: A defect in the roll potentiometer located in the captain's sidestick transducer unit, specifically a grease-filled groove in the potentiometer track near the neutral position, causing intermittent loss of contact and a voltage spike to the ELAC-1. 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

An A320 experienced uncommanded rolls on two consecutive days with autopilot engaged. Inspection found a defective roll potentiometer in the captain's sidestick transducer unit, leading to Airbus service bulletins.

Incident Overview

On two consecutive days, the same airplane experienced uncommanded rolls during flight with the autopilot engaged. The aircraft involved was an A320, as referenced in subsequent service bulletins. No other specific details about the operator, location, or date were provided.

Inspection Findings

Inspection of the airplane systems revealed a defect in a roll potentiometer located in the captain's sidestick transducer unit. A grease-filled groove was found in the potentiometer track near the neutral position. This potentiometer sends electronic signals to the elevator aileron controller (ELAC-1). The groove resulted in an intermittent loss of contact between the wiper and the track, which subsequently produced a voltage spike to the ELAC-1.

Manufacturer Response

Following this incident, Airbus issued two service bulletins addressing the voltage spike phenomenon. The bulletins noted that similar occurrences had been observed on other A320 airplanes since 1991. No further details on the content of the service bulletins were provided.

Technical Context

The roll potentiometer is a component within the sidestick transducer unit that converts mechanical input from the captain's sidestick into electronic signals for the flight control computers. The grease-filled groove caused abnormal resistance changes, leading to the uncommanded roll events. The voltage spike to the ELAC-1, which processes aileron and elevator commands, likely triggered the autopilot disengagement or incorrect roll response.

Probable cause

A defect in the roll potentiometer located in the captain's sidestick transducer unit, specifically a grease-filled groove in the potentiometer track near the neutral position, causing intermittent loss of contact and a voltage spike to the ELAC-1.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X03254. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.