What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
In preparation for a scheduled rotorcraft rating check ride, the pilot was practicing autorotation maneuvers in close proximity to, and north of, a bean field. The pilot stated that he was initiating the autorotation maneuver about 500 feet AGL in a direction towards the bean field and over an elevated railroad track. Due to a southerly headwind between the bean field and his position, while attempting to stretch the autorotation to clear the railroad track, he allowed the rotor speed to decay. During the recovery from the autorotation maneuver, the right skid contacted the bean stalks. While increasing the angle of attack for the recovery, and with the right skid in contact with the bean stalks, the helicopter dynamically rolled to the right. The rotor blades then contacted the ground and the helicopter came to rest on its right side. The ambient temperature was approximately 91 degrees (f) with high humidity. Substantial structural damage to the helicopter resulted as evidenced by the main and tail rotor blades separating and the buckling of the fuselage. No fire resulted and there was no injury to the pilot. No violation of regulations occurred.
As the FAA filed it
IN PREPARATION FOR A SCHEDULED ROTORCRAFT RATING CHECK RIDE, THE PILOT WAS PRACTICING AUTOROTATION MANEUVERS IN CLOSE PROXIMITY TO, AND NORTH OF, A BEAN FIELD. THE PILOT STATED THAT HE WAS INITIATING THE AUTOROTATION MANEUVER ABOUT 500 FEET AGL IN A DIRECTION TOWARDS THE BEAN FIELD AND OVER AN ELEVATED RAILROAD TRACK. DUE TO A SOUTHERLY HEADWIND BETWEEN THE BEAN FIELD AND HIS POSITION, WHILE ATTEMPTING TO STRETCH THE AUTOROTATION TO CLEAR THE RAILROAD TRACK, HE ALLOWED THE ROTOR SPEED TO DECAY. DURING THE RECOVERY FROM THE AUTOROTATION MANEUVER, THE RIGHT SKID CONTACTED THE BEAN STALKS. WHILE INCREASING THE ANGLE OF ATTACK FOR THE RECOVERY, AND WITH THE RIGHT SKID IN CONTACT WITH THE BEAN STALKS, THE HELICOPTER DYNAMICALLY ROLLED TO THE RIGHT. THE ROTOR BLADES THEN CONTACTED THE GROUND AND THE HELICOPTER CAME TO REST ON ITS RIGHT SIDE. THE AMBIENT TEMPERATURE WAS APPROXIMATELY 91 DEGREES (F) WITH HIGH HUMIDITY. SUBSTANTIAL STRUCTURAL DAMAGE TO THE HELICOPTER RESULTED AS EVIDENCED BY THE MAIN AND TAIL ROTOR BLADES SEPARATING AND THE BUCKLING OF THE FUSELAGE. NO FIRE RESULTED AND THERE WAS NO INJURY TO THE PILOT. NO VIOLATION OF REGULATIONS OCCURRED.
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 N9023Z · 2
Matched to the same aircraft by N-number and date.