N224VR

Substantial
None

Robinson R22 BETAS/N: 3038

Accident Details

Date
Monday, October 16, 2006
NTSB Number
DEN07CA013
Location
Monticello, UT
Event ID
20061121X01697
Coordinates
38.091110, -109.089447
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

an airframe vibration for reasons undetermined, resulting in the pilot performing a precautionary landing, and obstacle clearance not possible.

Aircraft Information

Registration
Make
ROBINSON
Serial Number
3038
Engine Type
Reciprocating
Year Built
2000
Model / ICAO
R22 BETAR22
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
2
FAA Model
R22 BETA

Registered Owner (Current)

Name
CONCHO AVIATION LLC
Address
PO BOX 747
City
STERLING CITY
State / Zip Code
TX 76951-0747
Country
United States

Analysis

On October 16, 2006, approximately 1210 mountain daylight time, a Robinson R22BETA, N224VR, registered to and piloted by an airline transport certificated pilot, was substantially damaged when the helicopter struck some scrub trees and terrain following uncontrollable yaw oscillations while in cruise flight approximately 18 miles northeast of Monticello, Utah. Visual meteorological conditions prevailed at the time of the accident. The business flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The pilot, the sole occupant aboard, was not injured. The local flight originated at Dove Creek, Colorado, approximately 1150, and was en route to Lisbon Valley, Utah.

According to the pilot's accident report and a verbal statement he gave to an FAA inspector, he was cruising at 8,500 feet msl (mean sea level) and at 65 KIAS (knots indicated airspeed) when he experienced a "slight yaw oscillation." The pilot decided to make a precautionary landing and initiated a descent. The oscillations increased to about one yaw per second. Before reaching the selected landing site, the "low-rotor RPM horn/light activated. When the pilot lowered the collective control to recover, he got an engine and rotor overspeed indication of 110 per cent. The pilot made a 180-degree turn and autorotated from 800 feet agl. The helicopter landed on rocky terrain, surrounded by pinon and juniper trees. Post-accident examination revealed the main rotor and tail rotor blades had struck trees. The tail rotor blades and gearbox separated from the tail boom.

According to a Robinson Helicopters repairman, he had found nothing that would explain the oscillations described by the pilot, or why the low-rotor RPM horn/light activated.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN07CA013