N47AH is a 1961 Bell 47G-3B. It is a rotorcraft with 3 seats, powered by a Lycoming TVO-435-GIA rated at 280 horsepower. The registration is active, with the registrant based in Le Sueur, MN. Its standard airworthiness certificate was issued in Apr 1993. It has been registered to its current owner since May 2005. This page also carries 2 NTSB events.
- 65 years old
- Only 16 Bell 47G-3B here
2005
1993
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N47AH's record changes.
According to the helicopter pilot, during an agricultural flight, he made a downwind turn to spray the intended field.
During the low airspeed right turn, he increased the engine power and the rotor RPM decreased.
He reported that he leveled the helicopter to clear powerline wires, but the rotor RPM remained low.
The helicopter descended, and the pilot landed the helicopter in a corn field.
The helicopter sustained substantial damage to the tailboom and the horizontal stabilizer.
The nearest METAR was 15 nautical miles south-southeast and reported that about the time of the accident, the wind was calm.
The pilot reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation.
On August 14, 2008, at 1045 central daylight time, a Bell helicopter 47G-3B, N47AH, collided with the terrain following a loss of control while taking off from a support truck in Kenyon, Minnesota. The pilot was not injured and the helicopter was substantially damaged. The aerial application flight was being operated under Title 14 Code of Federal Regulations Part 137. Visual meteorological conditions prevailed and no flight plan was filed. The local flight was originating at the time of the accident.
The pilot reported he had flown several aerial application flights earler in the day and that the humidity had increased as the weather cleared. He stated that the initial takeoff was normal. The pilot stated that when he was about 100 yards from the support truck, the rotor rpm began to decay and the helicopter settled into a soybean field. The spray boom caught in the crop and the helicopter pitched forward which resulted in the main rotor blades contacting the ground. The aft section of the tailboom, including the tail rotor, separated from the helicopter.
The pilot reported there was no mechanical malfunction/failure with the helicopter. He did report that he should have decreased his load due to the weather conditions.
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