N7095A

Substantial
None

ROBINSON HELICOPTER R22 BETAS/N: 2900

Accident Details

Date
Saturday, February 18, 2017
NTSB Number
WPR17LA068
Location
Holbrook, AZ
Event ID
20170228X65345
Coordinates
34.900001, -110.150001
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot’s failure to compensate for a loss of effective translational lift while turning from an upwind to a downwind condition at a low altitude and low airspeed, which resulted in a loss of helicopter control.

Aircraft Information

Registration
N7095A
Make
ROBINSON HELICOPTER
Serial Number
2900
Engine Type
Reciprocating
Year Built
1999
Model / ICAO
R22 BETAR22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
REIDHEAD KAMRON
Address
7121 HWY 180
Status
Deregistered
City
HOLBROOK
State / Zip Code
AZ 86025
Country
United States

Analysis

On February 18, 2017, about 0800 mountain standard time, the pilot of a Robinson R22 Beta, N7095A, experienced a loss of helicopter control while maneuvering in a turn and landed hard in an open field near Holbrook, Arizona. The private pilot/owner operated the helicopter under the provisions of 14 Code of Federal Regulations Part 91, as a personal flight. The pilot and one passenger were not injured. The helicopter was substantially damaged. Visual meteorological conditions prevailed for the local area flight and no flight plan had been filed. The flight departed from a private residence about 0715 the morning of the accident.

According to the pilot's written statement, he departed from his brother's residence about 0715 with the intent of flying around Holbrook on a personal flight. They over flew a cow pasture, and descended to look at the cows. The pilot reported his airspeed was about 10 knots with a 7-knot headwind. He maneuvered the helicopter in a 180-degree turn and the helicopter started an un-commanded descent. He pulled cyclic control, which responded by lowering engine and main rotor blade rpm; he tried to lower and increase throttle, and flared to land; however, the helicopter landed hard. The main rotor blades contacted and subsequently severed the tail boom.

The pilot stated that there were no mechanical anomalies that would have precluded normal operation of the helicopter.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR17LA068