Summary
On May 28, 2015, a Bell 47G 3B 1 (N112SH) was involved in an incident near Fort Pierre, SD. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's inadequate preflight fuel planning that resulted in a total loss of engine power due to fuel exhaustion, and the pilot's failure to maintain control of the helicopter during the subsequent autorotation landing.
The pilot reported that during cruise flight the helicopter's engine had a total loss of power and he made an emergency landing in a wheat field. He said the main rotor blades contacted the tail boom and sheared off the tail rotor during the landing. The helicopter sustained substantial damage to the tail rotor, tail rotor drive shaft, and tail boom. The pilot reported no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation.
The pilot reported using a placard as a reference for a fuel tank sight gauge. A postaccident examination by an FAA Aviation Safety Inspector revealed approximately three and one-half gallons of fuel in the right fuel tank and approximately one and one-half gallons of fuel in the left fuel tank.
This incident is documented in NTSB report GAA15CA097. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N112SH.
Accident Details
Probable Cause and Findings
The pilot's inadequate preflight fuel planning that resulted in a total loss of engine power due to fuel exhaustion, and the pilot's failure to maintain control of the helicopter during the subsequent autorotation landing.
Aircraft Information
Registered Owner (Current)
Analysis
The pilot reported that during cruise flight the helicopter's engine had a total loss of power and he made an emergency landing in a wheat field. He said the main rotor blades contacted the tail boom and sheared off the tail rotor during the landing. The helicopter sustained substantial damage to the tail rotor, tail rotor drive shaft, and tail boom. The pilot reported no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation.
The pilot reported using a placard as a reference for a fuel tank sight gauge. A postaccident examination by an FAA Aviation Safety Inspector revealed approximately three and one-half gallons of fuel in the right fuel tank and approximately one and one-half gallons of fuel in the left fuel tank. This make and model of helicopter has a capacity of 61 gallons of fuel of which 57.5 gallons of fuel is useable and three and one-half gallons of fuel are unusable.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# GAA15CA097