23.1505—Airspeed limitations.
        
        (c) 
         Paragraphs (a) and (b) of this section do not apply to turbine airplanes or to airplanes for which a design diving speed V
            D
            /M
            D is established under  § 23.335(b)(4). For those airplanes, a maximum operating limit speed (V
            MO
            /M
            MO -airspeed or Mach number, whichever is critical at a particular altitude) must be established as a speed that may not be deliberately exceeded in any regime of flight (climb, cruise, or descent) unless a higher speed is authorized for flight test or pilot training operations. V
            MO
            /M
            MO must be established so that it is not greater than the design cruising speed V
            C
            /M
            C and so that it is sufficiently below V
            D
            /M
            D and the maximum speed shown under  § 23.251 to make it highly improbable that the latter speeds will be inadvertently exceeded in operations. The speed margin between V
            MO
            /M
            MO and V
            D
            /M
            D or the maximum speed shown under  § 23.251 may not be less than the speed margin established between V
            C
            /M
            C and V
            D
            /M
            D under  § 23.335(b), or the speed margin found necessary in the flight test conducted under  § 23.253.