20181113022499A

Accident · Substantial damage

FAA accident report · Helicopteres Guimbal CABRI G2 · Newberg, OR · November 13, 2018

Date
November 13, 2018 · 09:49 local
Place
Newberg, OR
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Operator
SF8S
Damage
Substantial damage
Aircraft
N370PA
NTSB investigation
NTSBGAA19CA056
Reported as
Helicopteres Guimbal Cabri G2
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
1,552 total796 in this make and model107 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 a full down practice autorotation, the helicopter touched down with approximately 30 knots of ground speed. After ground contact, the helicopter started drifting right. The student pilot who was on-the-controls tried to correct the right drift by applying left pedal and left lateral cyclic. After a short period of time, the instructor got on the controls to assist in controlling the helicopter. The control inputs had no effect on controlling the slide of the helicopter. After sliding approximately 210 feet while drifting to the right, the helicopter contacted the sod on the right edge of the runway which caused it to spin 170 degrees with a right yaw and subsequently rolled onto its left side. During the maneuver, neither the flight instructor nor the student pilot noted any mechanical deficiencies with the helicopter.

As the FAA filed it

DURING A FULL DOWN PRACTICE AUTOROTATION, THE HELICOPTER TOUCHED DOWN WITH APPROXIMATELY 30 KNOTS OF GROUND SPEED. AFTER GROUND CONTACT, THE HELICOPTER STARTED DRIFTING RIGHT. THE STUDENT PILOT WHO WAS ON-THE-CONTROLS TRIED TO CORRECT THE RIGHT DRIFT BY APPLYING LEFT PEDAL AND LEFT LATERAL CYCLIC. AFTER A SHORT PERIOD OF TIME, THE INSTRUCTOR GOT ON THE CONTROLS TO ASSIST IN CONTROLLING THE HELICOPTER. THE CONTROL INPUTS HAD NO EFFECT ON CONTROLLING THE SLIDE OF THE HELICOPTER. AFTER SLIDING APPROXIMATELY 210 FEET WHILE DRIFTING TO THE RIGHT, THE HELICOPTER CONTACTED THE SOD ON THE RIGHT EDGE OF THE RUNWAY WHICH CAUSED IT TO SPIN 170 DEGREES WITH A RIGHT YAW AND SUBSEQUENTLY ROLLED ONTO ITS LEFT SIDE. DURING THE MANEUVER, NEITHER THE FLIGHT INSTRUCTOR NOR THE STUDENT PILOT NOTED ANY MECHANICAL DEFICIENCIES WITH THE HELICOPTER.

NTSB investigation

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