What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) The pilot reported that he was flying for about 10 minutes and making an approach to the metro west heliport just west of sus. On short final at about 100 ft AGL and 45 knots the helicopter began to shake violently. He lowered the collective to hasten his descent. He flared to reduce forward speed, leveled the aircraft and touched down. He landed on a wet dirt and grass surface. The shaking stopped after landing. He was able to perform a normal shut-down. During the whole event the flight controls seemed to react normally. The pilot stated that in previous flights he had experienced some unstabilized flight that might be considered like an out of track main rotor but never like this condition of severe vibration. A written statement by the pilot is attached to this report. Inspection of the helicopter found contact between a main rotor blade and a tail rotor blade. Damage to both blade tips resulted. No other damage to the helicopter was noted. It is believed this damage occurred on landing and was not the cause of the vibration.
As the FAA filed it
(-23) THE PILOT REPORTED THAT HE WAS FLYING FOR ABOUT 10 MINUTES AND MAKING AN APPROACH TO THE METRO WEST HELIPORT JUST WEST OF SUS. ON SHORT FINAL AT ABOUT 100 FT AGL AND 45 KNOTS THE HELICOPTER BEGAN TO SHAKE VIOLENTLY. HE LOWERED THE COLLECTIVE TO HASTEN HIS DESCENT. HE FLARED TO REDUCE FORWARD SPEED, LEVELED THE AIRCRAFT AND TOUCHED DOWN. HE LANDED ON A WET DIRT AND GRASS SURFACE. THE SHAKING STOPPED AFTER LANDING. HE WAS ABLE TO PERFORM A NORMAL SHUT-DOWN. DURING THE WHOLE EVENT THE FLIGHT CONTROLS SEEMED TO REACT NORMALLY. THE PILOT STATED THAT IN PREVIOUS FLIGHTS HE HAD EXPERIENCED SOME UNSTABILIZED FLIGHT THAT MIGHT BE CONSIDERED LIKE AN OUT OF TRACK MAIN ROTOR BUT NEVER LIKE THIS CONDITION OF SEVERE VIBRATION. A WRITTEN STATEMENT BY THE PILOT IS ATTACHED TO THIS REPORT. INSPECTION OF THE HELICOPTER FOUND CONTACT BETWEEN A MAIN ROTOR BLADE AND A TAIL ROTOR BLADE. DAMAGE TO BOTH BLADE TIPS RESULTED. NO OTHER DAMAGE TO THE HELICOPTER WAS NOTED. IT IS BELIEVED THIS DAMAGE OCCURRED ON LANDING AND WAS NOT THE CAUSE OF THE VIBRATION.