N496SB

Substantial
None

Boykin Rotorway Exec 162FS/N: 6992

Accident Details

Date
Sunday, March 25, 2007
NTSB Number
SEA07CA084
Location
Camarillo, CA
Event ID
20070409X00382
Coordinates
34.213890, -119.094444
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 maintain main rotor RPM resulting in an uncontrolled descent to a hard landing. A contributing factor was his lack of experience in make and model of aircraft.

Aircraft Information

Registration
Make
BOYKIN
Serial Number
6992
Engine Type
4-cycle
Year Built
2006
Model / ICAO
Rotorway Exec 162F
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
2
FAA Model
ROTORWAY EXEC 162F

Registered Owner (Current)

Name
BOYKIN STEPHEN V
Address
1884 CALLE YUCCA
City
THOUSAND OAKS
State / Zip Code
CA 91360-2253
Country
United States

Analysis

On March 25, 2007, at approximately 0855 Pacific daylight time, a Boykin Rotorway Exec 162F experimental, homebuilt helicopter, N496SB, was substantially damaged when it landed hard and rolled onto its left side. The commercial pilot, the sole occupant on board, was not injured. The helicopter was being operated by a private individual under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the local, personal flight that originated at approximately 0800. No flight plan had been filed.

The pilot said that this was his first solo flight in this make and model helicopter. He said he did weight and balance calculations before performing a preflight inspection of the aircraft. The pilot said that he performed a ground taxi, and hovered for 5 to 10 minutes, with pedal turns, to check the control capability. He flew to an open field and noted a slight drift to the left. He returned to the airport and made a normal approach to the helipad followed by a normal flare. The aircraft then started to drift to the left and would not correct with right cyclic; while trying to correct the left drift with right cyclic, the cyclic became limited by his leg and the confines of the cockpit. During an attempted go around, the pilot said that his airspeed had decreased to zero, and his rotor RPM had dropped. He said the helicopter began to descend and landed hard on the left forward skid. Subsequently the helicopter rolled onto its left side.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA07CA084