INDICATOR FOR AN AIRCRAFT CAPABLE OF HOVERING AND METHOD FOR ASSISTING PERFORMING A MANOEUVRE FOR THE AFORESAID AIRCRAFT

It is disclosed an indicator for an aircraft capable of hovering, comprising a first indication (36) associated to the value of vertical speed of the aircraft itself; the indicator comprises a first area wherein a second indication can be displayed that is associated to a Vortex Ring State condition being reached; the indicator comprises a second area wherein a third indication can be displayed that is associated to a Vortex Ring State condition approaching; wherein said second indication is overlapped to a first region of the first indication (35) corresponding to first values of a descent vertical speed and said third indication is overlapped to a second region of said first indication (35) corresponding to second values of said descent vertical speed, said first values being greater as an absolute value than said second values.