I have noticed slight drops in altitude with my P3 . Usually noticed when flying fast and doing hard turns, no where near as drastic as 10 feet. I attributed it to blade stall based on direction of travel and blade vortices . Someone above kinda touched on it but I think it is a result of the aerodynamics of the new design.
Maximum flight speeds of helicopters are limited by what is called retreating blade stall. As you approach velocity never exceed Vne the rotor blade retreating towards the rear of the aircraft will become less efficient and stall causing the aircraft to turn in the direction of the stall and loose altidude. Multi rotor aircraft with counter rotating blades are not affected to the same degree as the stall is counter balanced. It is the reason the Chinook was the fastest helicopter for a while.
I could be wrong but I suspect the new design is experiencing some sort of vortex disturbance causing one or more rotors to become less efficient based on flight direction and orientation .
Maximum flight speeds of helicopters are limited by what is called retreating blade stall. As you approach velocity never exceed Vne the rotor blade retreating towards the rear of the aircraft will become less efficient and stall causing the aircraft to turn in the direction of the stall and loose altidude. Multi rotor aircraft with counter rotating blades are not affected to the same degree as the stall is counter balanced. It is the reason the Chinook was the fastest helicopter for a while.
I could be wrong but I suspect the new design is experiencing some sort of vortex disturbance causing one or more rotors to become less efficient based on flight direction and orientation .