Pilot Debrief

ROBINSON HELICOPTER COMPANY R44 II near Dunlap, IL — 2015-04-15

Final reportCEN15LA198
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Date
2015-04-15
Location
Dunlap, IL, USA
Aircraft
ROBINSON HELICOPTER COMPANY R44 II
Registration
N754R
Category
Helicopter
Highest injury
None
Fatalities
0
Phase of flight
Maneuvering

Probable cause

A loss of main rotor rpm for reasons that could not be determined during postaccident examinations.

NTSB narrative

The commercial pilot stated he and the passenger were conducting a helicopter flight to observe and count geese at an altitude of 300 ft above the ground at an indicated airspeed of 60 knots. The pilot increased the collective to transition to another area when he noticed an increase in engine rpm and a decrease in rotor rpm along with the illumination of a main rotor warning light. The clutch warning light did not illuminate. The pilot initiated a downwind autorotation to a plowed field. The helicopter tipped forward on its skids, the main rotor contacted the ground, and the helicopter rolled over. Although a postaccident examination of the clutch and V-belts revealed some limited component wear, and some minor anomalies to the best tension actuator were noted, no anomalies were identified with the clutch system that would have resulted in a loss of main rotor rpm.

Analysis

Primary failure mode
Mechanical failure
First missed decision gate
Pilot could have chosen a different landing area to avoid rolling over.

NTSB coding

Evidence available

  • Photos
  • 7 docket documents
View NTSB final reportView NTSB docket

Docket documents7

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