DEN07CA013

NTSB accident investigation · Robinson R22 Beta · Monticello, UT · October 16, 2006

Accident · No injuriesData collectionFinal report
Date
October 16, 2006, 12:10 local (18:10 UTC)
Place
Monticello, UT
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N224VRRobinson R22 Beta
Weather
Visual (VMC) · Day
Status
Completed · report January 31, 2007
Report
Approved by Office Director
Parties
FAA Flight Standards District Office
FAA report
20061016022539A
Case key
64774

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Miscellaneous/otherCruise - normal
Airframe - vibration
Reason for occurrence undeterminedCause
In flight collision with objectLanding - flare/touchdown
Precautionary landing - initiatedPilot in command
Autorotation - attemptedPilot in command
Clearance - not possiblePilot in commandCause
Object - tree(s)
Terrain condition - mountainous/hilly

Analysis

The pilot said 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." He 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. Main and tail rotor and tail rotor blades struck the trees, separating the tail rotor blades and gearbox from the tail boom. According to the helicopter manufacturer, nothing was found that would explain the oscillations described by the pilot, or why the low-rotor RPM horn/light activated.

Factual narrative

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.

Aircraft

Registration
N224VR
Reported as
Robinson R22 Beta
Category
Helicopter
Serial number
3038
Airframe hours
1,472
Engine
Lycoming O-360-J2A, 145 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Registered owner
Cady L. Johnson
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 1, 2005 · 15 hours before
Departed
8V6 · Dove Creek, CO
Destination
NONE · Lisbon Valley, UT

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
54
Injuries
None
Certificates
Flight instructor, Airline transport, Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
December 1, 2005
Seat
Right
Flight hours
3,832 total · 1,143 in this make and model · 3,641 as pilot in command · 7 in the last 90 days · 7 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
40 statute miles
Lowest ceiling
None

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.