20190426003439A

Accident · Substantial damage

FAA accident report · Helicopteres Guimbal CABRI G2 · Mcminnville, OR · April 26, 2019

Date
April 26, 2019 · 17:00 local
Place
Mcminnville, OR
Airport
Mcminnville
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N367PA
NTSB investigation
NTSBGAA19CA226
Reported as
Helicopteres Guimbal Cabri G2
Reported engine
Lycoming O-360-J2A
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot
Pilot’s flight hours
729 total458 in this make and model92 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.

During the touch down portion of a practice, 180-degree, full-down autorotation, the helicopter contacted the ground with approximately 30 knots of ground speed, and began to drift to the right. The PIC stated he attempted to overcome the drift by applying left lateral cyclic and left pedal. PIC stated the control inputs had little effect on controlling the drift. The aircraft slid approximately 150 yards while drifting to the right, and the aircraft?s nose turning to the right, until making contact with the loose gravel on the right edge of the runway. Upon the aircraft skids making contact with the loose gravel, the aircraft rolled and came to rest on its left side. During the maneuver, the PIC reported no mechanical deficiencies with the aircraft.

As the FAA filed it

DURING THE TOUCH DOWN PORTION OF A PRACTICE, 180-DEGREE, FULL-DOWN AUTOROTATION, THE HELICOPTER CONTACTED THE GROUND WITH APPROXIMATELY 30 KNOTS OF GROUND SPEED, AND BEGAN TO DRIFT TO THE RIGHT. THE PIC STATED HE ATTEMPTED TO OVERCOME THE DRIFT BY APPLYING LEFT LATERAL CYCLIC AND LEFT PEDAL. PIC STATED THE CONTROL INPUTS HAD LITTLE EFFECT ON CONTROLLING THE DRIFT. THE AIRCRAFT SLID APPROXIMATELY 150 YARDS WHILE DRIFTING TO THE RIGHT, AND THE AIRCRAFT?S NOSE TURNING TO THE RIGHT, UNTIL MAKING CONTACT WITH THE LOOSE GRAVEL ON THE RIGHT EDGE OF THE RUNWAY. UPON THE AIRCRAFT SKIDS MAKING CONTACT WITH THE LOOSE GRAVEL, THE AIRCRAFT ROLLED AND CAME TO REST ON ITS LEFT SIDE. DURING THE MANEUVER, THE PIC REPORTED NO MECHANICAL DEFICIENCIES WITH THE AIRCRAFT.

NTSB investigation

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