UNREG

Substantial
None

BURNS Mini 500S/N: 001

Accident Details

Date
Friday, August 21, 2015
NTSB Number
CEN15LA396
Location
Butler, MO
Event ID
20150902X03440
Coordinates
38.289722, -94.340278
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to attain a proper landing flare following an autorotation for reasons that could not be determined based on available information.

Aircraft Information

Registration
UNREG
Make
BURNS
Serial Number
001
Model / ICAO
Mini 500

Analysis

On August 21, 2015, about 1100 central daylight time, an unregistered amateur-built Mini 500 helicopter, received substantial damage during a forced landing near Butler, Missouri, following a reported mechanical failure while in cruise flight. The pilot was not injured. During the mishap, the helicopter rolled onto its right side resulting in separation of the tail boom, and one of the main rotor blades. The aircraft was not registered to and was operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The flight originated from the Butler Memorial Airport (BUM), Butler, Missouri, about 1050.The pilot reported that he departed from runway 18 at BUM and remained in the traffic pattern. He said that on his second circuit he turned west from the downwind leg of the traffic pattern, crossed the runway and then turned north (right downwind for runway 18). He said that he was straight and level and the helicopter was operating normally when it suddenly shuddered and made a noise he described as sounding like a tire blowing out on a car. He performed an autorotation to a soybean field. He said that he leveled the helicopter about 5 feet above the ground, and about 2 feet above the soybean crop. He stated that he believed that the tail rotor contacted the crop causing some instability. The rotor speed bled off and the helicopter settled onto its right skid and rolled onto its side.

Postaccident examination of the helicopter failed to reveal any preimpact anomalies, however, complete examination of the power transmission system was not possible. In a telephone conversation with the pilot, he stated that when he initially experienced the problem, he thought the power transmission belts had failed, but upon examination after the accident he found they were still intact. When asked what he believed happened, he surmised that the one-way clutch that is part of the power transmission system had failed. He said that he had not taken anything apart on the helicopter and he did not think that he would.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN15LA396