20061016022539A

Accident · Substantial damage

FAA accident report · Robsin R22 BETA · Montrose, UT · October 16, 2006

Date
October 16, 2006 · 12:15 local
Place
Montrose, UT
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N224VR
NTSB investigation
NTSBDEN07CA013
Reported as
Robsin R22BETA
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,900 total1,175 in this make and model5 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Pilot experienced yaw oscillation approximately 15 minutes into the flight. Pilot began descending for a precautionary landing but before he reached the intended landing site the low rotor RPM horn and low rotor light illuminated followed by an engine/rotor overspeed as the collective was lowered. Pilot executed a 180 degree turn into the wind from approximately 800 ft. AGL to a clearing on the hillside.

As the FAA filed it

(-23) PILOT EXPERIENCED YAW OSCILLATION APPROXIMATELY 15 MINUTES INTO THE FLIGHT. PILOT BEGAN DESCENDING FOR A PRECAUTIONARY LANDING BUT BEFORE HE REACHED THE INTENDED LANDING SITE THE LOW ROTOR RPM HORN AND LOW ROTOR LIGHT ILLUMINATED FOLLOWED BY AN ENGINE/ROTOR OVERSPEED AS THE COLLECTIVE WAS LOWERED. PILOT EXECUTED A 180 DEGREE TURN INTO THE WIND FROM APPROXIMATELY 800 FT. AGL TO A CLEARING ON THE HILLSIDE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.