Casualties unknown

1999-04-01: Bell 206B (N992UC) — Papillon Grand Canyon Helicopt — Grand Canyon, AZ

Grand Canyon, AZ, US

On April 1, 1999, a Bell 206B (registration N992UC) operated by Papillon Grand Canyon Helicopt was involved in an aviation accident near Grand Canyon, AZ. Investigators recorded the probable cause as: The failure of the flight crew to properly preflight the helicopter and to detect and remove accumulated snow from the engine inlets and plenum chamber. 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 1781061362Data APIEditorial standards

A helicopter's engine stopped shortly after takeoff; during autorotation, a main rotor blade struck a tree, causing the helicopter to fall. The aircraft had been stored outside without engine inlet covers in cold, snowy conditions. Multiple start attempts preceded the flight.

Accident Sequence

Shortly after takeoff and transition to forward flight, the helicopter's engine stopped. During the ensuing autorotative landing glide, a main rotor blade struck a tree about 30 feet above ground level. The helicopter then fell to the ground.

Pre-flight Conditions

This was the first flight of the day. The helicopter had been stored outside overnight in conditions of cold temperatures and light snowfall without engine air inlet covers installed. Prior to the flight, the engine was difficult to start. Five start attempts were aborted before the engine was successfully started. During the first three start attempts, fuel was introduced, ignition occurred, the engine acceleration hung at 30 percent, and the starts were aborted.

After the third start attempt, a mechanic noted that the engine inlets were approximately half blocked by snow and cleared the snow from the inlets using a towel. He did not check the plenum chamber aft of the particle separator and forward of the engine inlet for snow.

Post-accident Examination

In the wreckage, the plenum chamber inspection window was found to be opaque. After the accident, another company mechanic who had dealt with the same starting difficulty on another helicopter of the same type parked under the same circumstances without inlet covers reported finding the plenum chamber of that helicopter contained several cups of snow.

The engine manufacturer reported that tests of the engine had shown that ingestion of as little as 6 ounces of snow or slush could flame out the engine.

Operational Context

The operator's procedure requiring that the last flight crew at the end of the day install the inlet covers on aircraft stored outside had not been followed.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001205X00484. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.