What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Pilot was circling a house for a real-estate agent to photograph house when he said he lost lift. He had just turned downwind and was approaching rising terrain that, from the photos taken during the flight, appeared to have trees rising to the level of his flight. The ground elevation was 5000'. Low, slow turning, acquiring a tail wind while unable to drop collective because of the raising terrain the helicopter lost translational lift, settled (with power) quickly, tail rotor struck a treetop separating the tail rotor drive shaft, tail rotor pitch control push rod, and tail rotor transmission. These parts were found in a counter-clockwise arch. The spinning helicopter hit the ground and rolled on its side making the accident survivable with only minor injuries. Robinson helicopter company safety notice SN-34 entitled "photo flights-very high risk" states that raising the collective to stop the descent in this situation can reduce RPM thereby reducing power available increasing descent rate with further loss of RPM and hence tail rotor effectiveness.
As the FAA filed it
(-23) PILOT WAS CIRCLING A HOUSE FOR A REAL-ESTATE AGENT TO PHOTOGRAPH HOUSE WHEN HE SAID HE LOST LIFT. HE HAD JUST TURNED DOWNWIND AND WAS APPROACHING RISING TERRAIN THAT, FROM THE PHOTOS TAKEN DURING THE FLIGHT, APPEARED TO HAVE TREES RISING TO THE LEVEL OF HIS FLIGHT. THE GROUND ELEVATION WAS 5000'. LOW, SLOW TURNING, ACQUIRING A TAIL WIND WHILE UNABLE TO DROP COLLECTIVE BECAUSE OF THE RAISING TERRAIN THE HELICOPTER LOST TRANSLATIONAL LIFT, SETTLED (WITH POWER) QUICKLY, TAIL ROTOR STRUCK A TREETOP SEPARATING THE TAIL ROTOR DRIVE SHAFT, TAIL ROTOR PITCH CONTROL PUSH ROD, AND TAIL ROTOR TRANSMISSION. THESE PARTS WERE FOUND IN A COUNTER-CLOCKWISE ARCH. THE SPINNING HELICOPTER HIT THE GROUND AND ROLLED ON ITS SIDE MAKING THE ACCIDENT SURVIVABLE WITH ONLY MINOR INJURIES. ROBINSON HELICOPTER COMPANY SAFETY NOTICE SN-34 ENTITLED "PHOTO FLIGHTS-VERY HIGH RISK" STATES THAT RAISING THE COLLECTIVE TO STOP THE DESCENT IN THIS SITUATION CAN REDUCE RPM THEREBY REDUCING POWER AVAILABLE INCREASING DESCENT RATE WITH FURTHER LOSS OF RPM AND HENCE TAIL ROTOR EFFECTIVENESS.
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 N90764 · 2
Matched to the same aircraft by N-number and date.