What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
During hover moved backward and left. Skid caught runway surface. Turned left and rolled over. (.4)the flight instructor asked the student to demonstrate an autorotation from a hover approximately 2 to 3 feet high. The CFI stayed on the controls throughout the maneuver. After they closed the throttle, the helicopter moved backwards and to the left. As the helicopter touched the ground, the rear portion of the left skid became imbedded in the runway surface and the aircraft rolled over onto its left side. The aircraft came to rest approximately 180 degrees from its original heading. The winds at the time were reported to be from a direction of 310 degrees at a velocity of 18 knots gusting to 22 knots. The CFI reported that they conducted all their maneuvers into the wind. (-23)while practicing hover autorotations the helicopter struck the ground while miving backwards and to the left. The left rear corner of the skid caught the surface of the runway and the momentum of the aircraft caused it to turn to the left and flip over and settler on its' left side. The winds were reported to be 18 knots gusting from 300 degrees. The aircraft was heading into the wind when the maneuver was initiated. The CFI indicated they were about 3 feet AGL and that the aircraft started the backwards and sideways movement just after, or at the same time they pulled back on the power. The CFI expected the skid to slide, but it did not, and caught the surface and flipped them over.
As the FAA filed it
DURING HOVER MOVED BACKWARD AND LEFT. SKID CAUGHT RUNWAY SURFACE. TURNED LEFT AND ROLLED OVER. (.4)THE FLIGHT INSTRUCTOR ASKED THE STUDENT TO DEMONSTRATE AN AUTOROTATION FROM A HOVER APPROXIMATELY 2 TO 3 FEET HIGH. THE CFI STAYED ON THE CONTROLS THROUGHOUT THE MANEUVER. AFTER THEY CLOSED THE THROTTLE, THE HELICOPTER MOVED BACKWARDS AND TO THE LEFT. AS THE HELICOPTER TOUCHED THE GROUND, THE REAR PORTION OF THE LEFT SKID BECAME IMBEDDED IN THE RUNWAY SURFACE AND THE AIRCRAFT ROLLED OVER ONTO ITS LEFT SIDE. THE AIRCRAFT CAME TO REST APPROXIMATELY 180 DEGREES FROM ITS ORIGINAL HEADING. THE WINDS AT THE TIME WERE REPORTED TO BE FROM A DIRECTION OF 310 DEGREES AT A VELOCITY OF 18 KNOTS GUSTING TO 22 KNOTS. THE CFI REPORTED THAT THEY CONDUCTED ALL THEIR MANEUVERS INTO THE WIND. (-23)WHILE PRACTICING HOVER AUTOROTATIONS THE HELICOPTER STRUCK THE GROUND WHILE MIVING BACKWARDS AND TO THE LEFT. THE LEFT REAR CORNER OF THE SKID CAUGHT THE SURFACE OF THE RUNWAY AND THE MOMENTUM OF THE AIRCRAFT CAUSED IT TO TURN TO THE LEFT AND FLIP OVER AND SETTLER ON ITS' LEFT SIDE. THE WINDS WERE REPORTED TO BE 18 KNOTS GUSTING FROM 300 DEGREES. THE AIRCRAFT WAS HEADING INTO THE WIND WHEN THE MANEUVER WAS INITIATED. THE CFI INDICATED THEY WERE ABOUT 3 FEET AGL AND THAT THE AIRCRAFT STARTED THE BACKWARDS AND SIDEWAYS MOVEMENT JUST AFTER, OR AT THE SAME TIME THEY PULLED BACK ON THE POWER. THE CFI EXPECTED THE SKID TO SLIDE, BUT IT DID NOT, AND CAUGHT THE SURFACE AND FLIPPED THEM OVER.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N2312N · 1
Matched to the same aircraft by N-number and date.