the invention is directed to a rotorcraft rotor equipped with a back (3).be the orientation of the axis of which is constant and training (6)the rotor is disposed laterally from the beam.tail of the aircraft. a mechanism for manoeuvring (14) of the blades (8).the tail rotor (3) includes a set of control point (27)placed with the blades (8), and a stem manceuvrablecontrol (21) oriented along the axis of the tail rotor (6).(3). the set of control (27) is disposed in a planemontage (pm), causing a continuous constant cyclic variationthe rotor blades (8). a man can turn the stem(21) modifies the control operation of the cyclic variationnot permanent blades (8) between an input of buoyancy andcontribution of rotorcraft propulsion in the orientation in translationcornerstone of the control shelf (27) in the assembly plan(pm).
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