What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On 8/05/03, at approximately 1300 PDT, roy w. pettit, commercial certificate 548350340, PIC of N9254Y, a bht 206BIII helicopter, operating under 14CFR91, crashed during attempted landing at a residential construction site in Merced, CA. The pilot and two passengers were uninjured. The aircraft was substantially damaged. The pilot conducted a steep approach to a 12'X12', 4" high, concrete pad, and landed with the forward third of the skids on the pad. The helicopter tilted tail low striking the tail guard on the ground. The pilot attempted to correct the rearward tilt with forward cyclic and a rapid increase of collective pitch. The helicopter lifted off the pad to approximately 5 feet to 10 feet and accelerated forward in a nose low attitude. The aircraft rolled hard right impacting the ground on the toe of the right skid. The advancing main rotor blade struck the ground and the helicopter came to rest on its right side. Inspection determined the flight control system was intact and functioning properly and was not a causal factor.
As the FAA filed it
(-23) ON 8/05/03, AT APPROXIMATELY 1300 PDT, ROY W. PETTIT, COMMERCIAL CERTIFICATE 548350340, PIC OF N9254Y, A BHT 206BIII HELICOPTER, OPERATING UNDER 14CFR91, CRASHED DURING ATTEMPTED LANDING AT A RESIDENTIAL CONSTRUCTION SITE IN MERCED, CA. THE PILOT AND TWO PASSENGERS WERE UNINJURED. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED. THE PILOT CONDUCTED A STEEP APPROACH TO A 12'X12', 4" HIGH, CONCRETE PAD, AND LANDED WITH THE FORWARD THIRD OF THE SKIDS ON THE PAD. THE HELICOPTER TILTED TAIL LOW STRIKING THE TAIL GUARD ON THE GROUND. THE PILOT ATTEMPTED TO CORRECT THE REARWARD TILT WITH FORWARD CYCLIC AND A RAPID INCREASE OF COLLECTIVE PITCH. THE HELICOPTER LIFTED OFF THE PAD TO APPROXIMATELY 5 FEET TO 10 FEET AND ACCELERATED FORWARD IN A NOSE LOW ATTITUDE. THE AIRCRAFT ROLLED HARD RIGHT IMPACTING THE GROUND ON THE TOE OF THE RIGHT SKID. THE ADVANCING MAIN ROTOR BLADE STRUCK THE GROUND AND THE HELICOPTER CAME TO REST ON ITS RIGHT SIDE. INSPECTION DETERMINED THE FLIGHT CONTROL SYSTEM WAS INTACT AND FUNCTIONING PROPERLY AND WAS NOT A CAUSAL FACTOR.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.