To: BlenderPilot
You used the term stalls. Bell may have interpreted this as compressor stalls, which in truth may have been the case. If you have experienced a compressor stall the entire driveline and dynamic system is changed (but only after a detailed inspection). We experienced compressor stalls on our 214s in Iran and the same was true for them when a compressor stall happened. In some cases parts of the fuselage were changed. Of course there is a big difference in the horsepower of the 206 and the 214 engines with the application of instantaneous torque being applied to the respective drivetrains and dynamics.
I don’t know the design geometry of the 206 but how can a blade hit a fin. Is there a possibility that the transmission tilted backwards when the helicopter nosed over and the pilot may have pulled aft cyclic.
