Casualties unknown

2002-05-22: Robinson R22 BETA (N7194J) — Mammoth Lakes, CA

Mammoth Lakes, CA, US

On May 22, 2002, a Robinson R22 BETA (registration N7194J) was involved in an aviation accident near Mammoth Lakes, CA. Investigators recorded the probable cause as: The aircraft was operated at a gross weight exceeding its maximum allowable limit during flight in high density altitude conditions. 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

A helicopter crashed into trees and mountainous terrain approximately 7.8 miles from the airport after departing with weight exceeding its maximum allowable limits.

What happened

Prior to departure, the Robinson R22 (implied type based on context of flight manual references) had its main and auxiliary fuel tanks topped off. Witnesses observed the pilot and passenger board the aircraft and noted a normal engine start. After idling for two minutes, the engine RPM increased to full power. The helicopter initially lifted approximately 3 to 4 feet before setting down in a controlled manner. Following a brief decrease in RPM, the engine returned to full power. The aircraft then lifted off, turned west, and moved about 30 feet toward a closed taxiway marked with a yellow X, where it set down heavily. Witnesses reported difficulty attempting to maintain lift. After several seconds, the helicopter lifted again, dragging the forward portion of the skids on the taxiway, and departed to the west without gaining significant altitude. The aircraft subsequently impacted trees and rising mountainous terrain approximately 7.8 miles from the airport.

The investigation

The investigation determined that the helicopter's gross weight at the time of departure was 1,459.25 lbs, which exceeded the maximum allowable gross weight of 1,370 lbs. This weight included the occupants, baggage, and full fuel tanks. Environmental conditions played a significant role, as the density altitude at the departure airport was calculated at 8,702 feet, while the accident site was at 10,681 feet. The investigation noted that performance specifications for in-ground-effect (IGE) and out-of-ground-effect (OGE) hover ceilings were not available for weights exceeding the 1,370 lbs limit. An engine test run performed on the airframe revealed no anomalies or discrepancies.

Probable cause

The aircraft was operated at a gross weight exceeding its maximum allowable limit during flight in high density altitude conditions.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020531X00796. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.