Casualties unknown

Landing Gear Collapse After Electrical Short Attributed to Soda Spill (N396AE)

Lawton, OK, US

On February 22, 1998, a Saab-scania AB (saab) 340B (registration N396AE) operated by Simmons Airlines was involved in an aviation accident near Lawton, OK. Investigators recorded the probable cause as: Electrical short in the weight-on-wheels relay attributed to a soda spill on a previous flight. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

During cruise, a twin-engine transport aircraft's landing gear control circuit breaker popped after an odor of burning electrical equipment was detected. The left main gear collapsed on landing after the crew landed with unsafe indications. Investigation attributed the short to a prior soda spill and noted an unsealed cockpit floor.

Incident Description

During cruise flight, the flight crew detected an odor resembling burning or smoldering electrical equipment. The landing gear control circuit breaker had popped. The crew consulted the company's Quick Reference Handbook (QRH), which addressed hydraulic problems but did not discuss electrical problems related to landing gear operation. The company's maintenance facility was informed, but the maintenance person on duty could not assist the flight crew.

Flight Crew Actions

Three tower fly-bys were conducted. The flight attendant and tower personnel reported that the landing gear appeared to be down with the gear doors closed. The flight crew elected to land with the landing gear handle light indicating an 'in-transit' condition and both main landing gear indicators showing an 'unsafe' condition. During the landing roll, the left main landing gear of the twin-engine transport category airplane collapsed.

Examination Findings

Post-incident examination revealed that the weight-on-wheels relay, located in the avionics bay directly under the captain's station, had shorted. This short caused the landing gear control circuit breaker to pop. The electrical short was attributed to the spill of a soda can on the flight deck on a previous flight. The investigation also revealed that the cockpit floor was not carpeted or sealed to prevent fluids or moisture from seeping into the electrical compartment beneath the cockpit floor.

Emergency Extension System Review

A review of the airplane's emergency extension system showed that the landing gear could have been extended if the flight crew had pulled the emergency extension handle.

Probable cause

Electrical short in the weight-on-wheels relay attributed to a soda spill on a previous flight.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X09539. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.