ROBINSON HELICOPTER COMPANY R44 II

Prairie Lea, TX — July 16, 2015

Event Information

DateJuly 16, 2015
Event TypeACC
NTSB NumberGAA15CA232
Event ID20150819X72333
LocationPrairie Lea, TX
CountryUSA
Coordinates29.71305, -97.77639
Highest InjuryMINR

Aircraft

MakeROBINSON HELICOPTER COMPANY
ModelR44 II
CategoryHELI
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor3
None0
Total Injured3

Event Location

Probable Cause

The pilot's failure to maintain rotor rpm, resulting in an uncontrolled descent and collision with trees.

Full Narrative

The helicopter pilot reported that while flying at a low altitude and low airspeed, over tree-covered terrain, he made a steep left turn downwind, and the low rotor rpm horn sounded. He stated that he lowered the collective slightly and rolled on throttle, but the helicopter descended and impacted trees and terrain.

The pilot reported that he completed a damage assessment and flew the helicopter to his home airport without further incident. Substantial damage was sustained to the helicopter left aft fuselage frame assembly. The pilot reported that there were no mechanical malfunctions or anomalies prior to or during the flight that would have prevented normal helicopter operation.

ADDITIONAL INFORMATION

Vortex Ring State (Commonly known as "settling with power")

FAA-H-8023-21A identifies, "A vortex ring state may be entered during any maneuver that places the main rotor in a condition of descending in a column of disturbed air and low forward airspeed. Airspeeds that are below translational lift airspeeds are within this region of susceptibility to settling with power aerodynamics (pg. 11-10)."

"Some of the situations that are conducive to a settling with power condition are: any hover above ground effect altitude, specifically attempting to hover OGE at altitudes above the hovering ceiling of the helicopter, attempting to hover OGE without maintaining precise altitude control, pinnacle or rooftop helipads when the wind is not aligned with the landing direction, and downwind and steep power approaches in which airspeed is permitted to drop below 10 knots depending on the type of helicopter (pg. 11-10)."

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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