Originally Posted by
JohnDixson
Gray posted in part: “The manufacturer does not consider servo transparency a failure of the system, but a limitation of all single hydraulic systems”
Thanks for the AH statement, but I’m missing something. If the single servo system was designed to provide a control force which exceeds the maximum forces that can be generated by the rotor, this discussion, and the similar one for the Gazelle, would be moot, n’est-ce pas?
talk to airbus, not me. it's their quote