N7058Z

Substantial
Minor

ROBINSON HELICOPTER R22 BETAS/N: 2896

Accident Details

Date
Saturday, November 14, 2015
NTSB Number
CEN16LA040
Location
Sugarland, TX
Event ID
20151030X93614
Coordinates
29.882223, -95.916946
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The overspeed of the main rotor system for reasons that could not be determined based on the available information.

Aircraft Information

Registration
N7058Z
Make
ROBINSON HELICOPTER
Serial Number
2896
Engine Type
Reciprocating
Year Built
1998
Model / ICAO
R22 BETAR22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
AAROW AIRCRAFT LEASING LLC
Address
3824 CEDAR SPRINGS RD # 801-9127
Status
Deregistered
City
DALLAS
State / Zip Code
TX 75219-4136
Country
United States

Analysis

On November 14, 2015, about 0950 central standard time, a Robinson R22 Beta helicopter, N7058Z, experienced a hard landing following an autorotation near Sugarland, Texas. The private rated pilot sustained minor injuries and the helicopter was substantially damaged. The helicopter was registered to Jerry Trimble Helicopters and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which operated without a flight plan.According to the pilot, after flying for about 50 minutes the main rotor rpm over-sped, and went to the top of the gauge. The pilot reduced throttle but was unable to get the rotor rpms within limits, so he initiated an autorotation. The pilot maneuvered the helicopter to an open field location and landed hard. After the initial impact, the helicopter rolled on to its left side. The tail boom was severed from the fuselage during the impact, and was displaced about 150 feet from the fuselage.

The pilot reported that the helicopter's rotor had over sped about 2 weeks prior to the accident. A 50-hour inspection of the helicopter did not reveal a reason for the main rotor over speed. The pilot suspected a mechanical malfunction resulting in an over speed of the rotor system. A visual examination of the helicopter by inspectors from the Federal Aviation Administration did not reveal any anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN16LA040