Casualties unknown

1982-07-05: Douglas DC-9-31 (N919RW) — Republic Airlines West, Inc. — Boise, ID

Boise, ID, US

On July 5, 1982, a Douglas DC-9-31 (registration N919RW) operated by Republic Airlines West, Inc. was involved in an aviation accident near Boise, ID. Investigators recorded the probable cause as: Malfunction of the right flap position transmitter due to corrosion, causing an erroneous flap setting signal to the stall warning computer and subsequent activation of the stickshaker/stall warning system at incorrect airspeeds. 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 1781061362Data APIEditorial standards
Aircraft registered N919RW
Aircraft registered N919RW. Photo: Pete Macklin / CC BY-SA 2.0, via Wikimedia Commons

A flight aborted takeoff after stick shaker activation, resulting in a runway overrun. Investigation found a corroded right flap position transmitter caused erroneous stall warnings.

Incident Overview

After a gate delay to accommodate late passengers, the flight received clearance for takeoff on Runway 28L. Approximately four seconds after rotation speed was called, the stickshaker activated, prompting the crew to abort the takeoff. A cockpit voice recorder (CVR) readout indicated that the thrust reversers were deployed 11 seconds later. The aircraft came to a stop in the dirt overrun, about 50 feet beyond the end of the runway.

Damage and Injuries

The aircraft sustained only minor damage, and no injuries were reported.

Investigation Findings

Prior to its departure from Seattle, Washington, the aircraft had been placarded for an inoperative anti-skid system. The investigation revealed that the right flap position transmitter had malfunctioned due to corrosion. According to the investigation, a malfunction of either flap position transmitter can send an erroneous flap setting signal to the stall warning computer. This, in turn, activates the stickshaker/stall warning system at incorrect airspeeds.

Probable cause

Malfunction of the right flap position transmitter due to corrosion, causing an erroneous flap setting signal to the stall warning computer and subsequent activation of the stickshaker/stall warning system at incorrect airspeeds.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020917X04180. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.