What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Mr. Leloup was conducting a cherry drying operation under part 91 at the munson cherry farm. He turned at the end of a run and caught the Bell 206B'S tail rotor on a power transmission wire, which wrapped around the tail rotor shaft. Mr. Leloup felt the bump and headed for a more open spot in the orchard, but the power wire stayed attached to the ship and kept him from the open spot. The ship, having lost tail rotor authority, began to drift right and banked 15 degrees, wherein Mr. Leloup corrected the bank with stick input and set the helicopter down on its skids impacting two mature cherry trees. The main rotor blades impacted the cherry trees, shattering. The transmission and rotor head assembly ripped out the helicopter and landed some 20 feet ahead of the machine. Portions of the cherry tree impacted the helicopter around the engine and transmission bay damaging the deck and deck sides. The fuselage and tail boom assembly shows stress with dents, bends and kinks in structural members.
As the FAA filed it
(-23) MR. LELOUP WAS CONDUCTING A CHERRY DRYING OPERATION UNDER PART 91 AT THE MUNSON CHERRY FARM. HE TURNED AT THE END OF A RUN AND CAUGHT THE BELL 206B'S TAIL ROTOR ON A POWER TRANSMISSION WIRE, WHICH WRAPPED AROUND THE TAIL ROTOR SHAFT. MR. LELOUP FELT THE BUMP AND HEADED FOR A MORE OPEN SPOT IN THE ORCHARD, BUT THE POWER WIRE STAYED ATTACHED TO THE SHIP AND KEPT HIM FROM THE OPEN SPOT. THE SHIP, HAVING LOST TAIL ROTOR AUTHORITY, BEGAN TO DRIFT RIGHT AND BANKED 15 DEGREES, WHEREIN MR. LELOUP CORRECTED THE BANK WITH STICK INPUT AND SET THE HELICOPTER DOWN ON ITS SKIDS IMPACTING TWO MATURE CHERRY TREES. THE MAIN ROTOR BLADES IMPACTED THE CHERRY TREES, SHATTERING. THE TRANSMISSION AND ROTOR HEAD ASSEMBLY RIPPED OUT THE HELICOPTER AND LANDED SOME 20 FEET AHEAD OF THE MACHINE. PORTIONS OF THE CHERRY TREE IMPACTED THE HELICOPTER AROUND THE ENGINE AND TRANSMISSION BAY DAMAGING THE DECK AND DECK SIDES. THE FUSELAGE AND TAIL BOOM ASSEMBLY SHOWS STRESS WITH DENTS, BENDS AND KINKS IN STRUCTURAL MEMBERS.
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 N213SD · 1
Matched to the same aircraft by N-number and date.