helicopter nose up pitch up attitude
you are right at the time of take off it will be mid-aft CG then depending on the type of mission at the time of landing it will go further AFT CG. So in all probability there will be some allowable nose up pitch attitude subject to tail guard inclination w.r.t skid. In some light helicopters like tail rotor mounted on longitudinal axis, what will be the limiting nose up pitch attitude at the time of landing/takeoff. Am looking for Augusta 119, Bell 407 AND 429, eurocopter AS350 and Aérospatiale Alouette helicopter data. Some body from forums can help me in getting these data.