Casualties unknown

Engine Power Interruptions and Airspeed Indication Failures During Flight in Icing Conditions (N245AE)

Nashville, TN, US

On May 3, 1994, a Saab-scania AB (saab) S340B (registration N245AE) operated by Wings West Airlines, Inc. was involved in an aviation accident near Nashville, TN. Investigators recorded the probable cause as: Ice or slush accumulation on the engine inlet particle separator that could break off and enter the engine, causing engine flameout. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 4 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

An aircraft experienced engine power interruptions in both engines and loss of airspeed indications during cruise in icing conditions. The flight crew declared an emergency and landed safely. Investigation revealed ice accumulation on engine inlet particle separators as the cause.

Flight Events

The aircraft had been parked on the ramp overnight, uncovered, in continuous rain. Takeoff was conducted in heavy rain. After reaching cruising altitude at flight level 250, the crew experienced power interruptions in both engines. The flight conditions included instrument meteorological conditions, an outside air temperature of -20 degrees Celsius, and light rime icing. Additionally, all airspeed indications decreased to zero. The flight crew initiated a descent and declared an emergency. The aircraft was landed safely at its destination.

Investigation Findings

The investigation determined that engine power interruptions had occurred in light icing conditions since the aircraft was introduced into revenue service. Airworthiness directives were issued, first prohibiting revenue flights and later restricting flights in icing conditions unless the aircraft was equipped with an auto ignition system. The manufacturer found that ice or slush could accumulate on the engine inlet particle separator, break off, and enter the engine, resulting in a flameout. This accumulation was not visible to the pilots and was not alleviated by engine anti-ice systems. An auto ignition system was subsequently added that could restart an engine within two seconds.

Certification Implications

Aircraft certification rules require that no accumulation of ice on engine inlets occurs that would adversely affect engine operation. The findings from this event highlighted a deficiency in meeting that requirement under certain conditions.

Probable cause

Ice or slush accumulation on the engine inlet particle separator that could break off and enter the engine, causing engine flameout.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X01205. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.