This time as the helicopter was once again about 30 feet from touchdown, it began spinning to the left and impacted the ground. Builder questions are welcome and can be sent either through email or by phone. One person died Sunday when the small helicopter he was flying crashed into a hillside near Dearborn. We will pay $3000.00 for the dwgs! But I'm back. Body and structure are the same to minimize weight and maximize structural efficiency. All materials are provided including the blades and the instruments. The Swift kit helicopter will have a useful load of 700 lbs with a maximum speed of 120 mph, and a cruise range of up to 350 miles. He also stated that he thought that the previous flight when it spun, that he believed he came in a little too fast and since the governor did not really work to well and the helicopter did not have a lot of horsepower to correct or recover that could have caused the spins. The pilot must hold a Federal Aviation Administration (FAA) pilot certification for rotorcraft and a FAA medical certificate to operate the helicopter. - The correlator was adjusted for maximum throttle change for collective control movement. 3 sprocket was connected to the secondary drive system. Because of rotor blade and drive train inertia, the correlator would act before the fact and would increase or decrease the engine power before the engine actually "felt" the load change. When the system was first engaged by turning on the governor switch on the control module, the engine rpm and position of the magnetic clutch magnet are unknown. This provides the high strength to weight ratio and reliability required in an ultralight helicopter. The microcontroller would then detect the rpm at which the engine was turning, and then would store that rpm in memory as the Set Point rpm. Eight aircraft are currently under restoration. The joystick is floor mounted. Any suggestions pls? CASCADE, MT. Operation of the helicopter by an inadequately trained pilot could result in severe injury or death. According to an FAA inspector, the pilot advised him while hospitalized that after takeoff, while flying about twice the height of powerlines in a westerly direction over a field, the helicopter experienced a partial loss of engine power. A postcrash fire then ensued. Will pay for this as we are converting to a gyro-copter but need the controls and drive assy composite wont help us coz of the liabilities or competition!!! On the day of the accident, the pilot had trailered the helicopter into the park to do some flying in the local area. The helicopter must be operated with floats installed in order to be in compliance with the 14 Code of Federal Regulations Part 103 weight restrictions limit. There were signatures of tree damage where the broken tail boom section and gear box were thrown away from the main wreckage site. During the accident the pilot had been seriously injured, suffered memory loss and for approximately a year and a half was unable to communicate with NTSB investigators. But I did not actually fo ahead and buy one because unlike my several Cubs, there is a constant work load.
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