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 transporting a previously crashed Piper PA-18 airplane on a 100 foot external load line. The external load line was attached to a spreader bar that was attached to the wing structure of the airplane. The pilot stated that he was flying about 60 knots, and about 2,000 feet above ground level (AGL), when he felt the load shift. He indicated that it felt as if the suspended airplane became light, or unloaded, and he immediately began to slow the helicopter's airspeed. The helicopter then suddenly pitched nose-down about 45 degrees. The tail boom of the helicopter was struck by one or more main rotor blades, severing the tail rotor drive shaft, and one or more of the main rotor hub spacing cables broke at their frangible bolt attach points. The pilot said that about 1,000 feet AGL, he shut the engine off, and performed a touch down autorotation. During the landing on soft tundra, one of the main landing gear wheels dug into the terrain, and the helicopter's tail boom was struck by the main rotor blades, severing about two feet of the aft end of the tail boom. The pilot has not determined the cause of the external load shift.
As the FAA filed it
(-23) THE PILOT REPORTED THAT HE WAS TRANSPORTING A PREVIOUSLY CRASHED PIPER PA-18 AIRPLANE ON A 100 FOOT EXTERNAL LOAD LINE. THE EXTERNAL LOAD LINE WAS ATTACHED TO A SPREADER BAR THAT WAS ATTACHED TO THE WING STRUCTURE OF THE AIRPLANE. THE PILOT STATED THAT HE WAS FLYING ABOUT 60 KNOTS, AND ABOUT 2,000 FEET ABOVE GROUND LEVEL (AGL), WHEN HE FELT THE LOAD SHIFT. HE INDICATED THAT IT FELT AS IF THE SUSPENDED AIRPLANE BECAME LIGHT, OR UNLOADED, AND HE IMMEDIATELY BEGAN TO SLOW THE HELICOPTER'S AIRSPEED. THE HELICOPTER THEN SUDDENLY PITCHED NOSE-DOWN ABOUT 45 DEGREES. THE TAIL BOOM OF THE HELICOPTER WAS STRUCK BY ONE OR MORE MAIN ROTOR BLADES, SEVERING THE TAIL ROTOR DRIVE SHAFT, AND ONE OR MORE OF THE MAIN ROTOR HUB SPACING CABLES BROKE AT THEIR FRANGIBLE BOLT ATTACH POINTS. THE PILOT SAID THAT ABOUT 1,000 FEET AGL, HE SHUT THE ENGINE OFF, AND PERFORMED A TOUCH DOWN AUTOROTATION. DURING THE LANDING ON SOFT TUNDRA, ONE OF THE MAIN LANDING GEAR WHEELS DUG INTO THE TERRAIN, AND THE HELICOPTER'S TAIL BOOM WAS STRUCK BY THE MAIN ROTOR BLADES, SEVERING ABOUT TWO FEET OF THE AFT END OF THE TAIL BOOM. THE PILOT HAS NOT DETERMINED THE CAUSE OF THE EXTERNAL LOAD SHIFT.
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 N119PH · 1
Matched to the same aircraft by N-number and date.