20100217027599A

Accident · Substantial damage

FAA accident report · Robinson He R22 BETA · Parlier, CA · February 17, 2010

Date
February 17, 2010 · 14:37 local
Place
Parlier, CA
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N313DA
NTSB investigation
NTSBWPR10LA138
Reported as
Robinson He R22 Beta
Reported engine
Lycoming O-360 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
1,702 total64 in this make and model38 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.

On February 17, 2010 at 1450 PDT , N313DA a Robinson R22 helicopter , made a forced landing in a field near Parlier, CA. The commercial pilot stated that he was flying straight and level when suddenly the helicopter pitched forward and immediately rolled inverted to the right. The pilot was able to regain control when he applied aft cyclic and lowered the collective recovering from the low-g maneuver and landed the helicopter in a field. A rotor blade ( red marked) struck the tail boom as the main rotor blades slowed down. . Substantial damage to the main rotor blade hub indicated that this helicopter encountered a low-g condition

As the FAA filed it

ON FEBRUARY 17, 2010 AT 1450 PDT , N313DA A ROBINSON R22 HELICOPTER , MADE A FORCED LANDING IN A FIELD NEAR PARLIER, CA. THE COMMERCIAL PILOT STATED THAT HE WAS FLYING STRAIGHT AND LEVEL WHEN SUDDENLY THE HELICOPTER PITCHED FORWARD AND IMMEDIATELY ROLLED INVERTED TO THE RIGHT. THE PILOT WAS ABLE TO REGAIN CONTROL WHEN HE APPLIED AFT CYCLIC AND LOWERED THE COLLECTIVE RECOVERING FROM THE LOW-G MANEUVER AND LANDED THE HELICOPTER IN A FIELD. A ROTOR BLADE ( RED MARKED) STRUCK THE TAIL BOOM AS THE MAIN ROTOR BLADES SLOWED DOWN. . SUBSTANTIAL DAMAGE TO THE MAIN ROTOR BLADE HUB INDICATED THAT THIS HELICOPTER ENCOUNTERED A LOW-G CONDITION

NTSB investigation

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