What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
The pilot preflighted the helicopter on Friday morning before flying it 65 NM from his home to F14, about a 20 minute flight. He landed and meet with his CFI. After another preflight and servicing the helicopter, they took off to practice autorotations in the traffic pattern. After 5 practice auto rotations to the side of runway 30 terminating with power recoveries, they set-up for a hydraulics off run-on landing. They expanded their traffic pattern, planning on a touchdown on runway 30. The engine quit as the hydraulics were being turned off. They were too FAR out on final to make it to runway 30 at F14. The pilot turned the controls over to the CFI who turned left to autorotate into an open field. They lost rotor RPM as they crossed over a utility wire on the east edge of the landing site. Half of the lower tail fin (vertical stabilizer) was sliced off as it cut through that wire. With low rotor RPM and a high sink rate the main rotor deflected during touchdown and cut off the tailboom. The helicopter reversed direction and rested on it?s right side. The skids were torn off in the soft marshy ground. There was no post-crash fire.
As the FAA filed it
THE PILOT PREFLIGHTED THE HELICOPTER ON FRIDAY MORNING BEFORE FLYING IT 65 NM FROM HIS HOME TO F14, ABOUT A 20 MINUTE FLIGHT. HE LANDED AND MEET WITH HIS CFI. AFTER ANOTHER PREFLIGHT AND SERVICING THE HELICOPTER, THEY TOOK OFF TO PRACTICE AUTOROTATIONS IN THE TRAFFIC PATTERN. AFTER 5 PRACTICE AUTO ROTATIONS TO THE SIDE OF RUNWAY 30 TERMINATING WITH POWER RECOVERIES, THEY SET-UP FOR A HYDRAULICS OFF RUN-ON LANDING. THEY EXPANDED THEIR TRAFFIC PATTERN, PLANNING ON A TOUCHDOWN ON RUNWAY 30. THE ENGINE QUIT AS THE HYDRAULICS WERE BEING TURNED OFF. THEY WERE TOO FAR OUT ON FINAL TO MAKE IT TO RUNWAY 30 AT F14. THE PILOT TURNED THE CONTROLS OVER TO THE CFI WHO TURNED LEFT TO AUTOROTATE INTO AN OPEN FIELD. THEY LOST ROTOR RPM AS THEY CROSSED OVER A UTILITY WIRE ON THE EAST EDGE OF THE LANDING SITE. HALF OF THE LOWER TAIL FIN (VERTICAL STABILIZER) WAS SLICED OFF AS IT CUT THROUGH THAT WIRE. WITH LOW ROTOR RPM AND A HIGH SINK RATE THE MAIN ROTOR DEFLECTED DURING TOUCHDOWN AND CUT OFF THE TAILBOOM. THE HELICOPTER REVERSED DIRECTION AND RESTED ON IT?S RIGHT SIDE. THE SKIDS WERE TORN OFF IN THE SOFT MARSHY GROUND. THERE WAS NO POST-CRASH FIRE.
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 N1159W · 2
Matched to the same aircraft by N-number and date.