Performance information.

CFR · 2024-01-01 · US · Title 14

Flight manual performance information which exceeds any operating limitation may be shown only to the extent necessary for presentation clarity or to determine the effects of approved optional equipment or procedures. When data beyond operating limits are shown, the limits must be clearly indicated. The following must be provided: (a) (1) The indicated airspeeds corresponding with those determined for takeoff, and the procedures to be followed if the critical engine fails during takeoff; (2) The airspeed calibrations; (3) The techniques, associated airspeeds, and rates of descent for autorotative landings; (4) The rejected takeoff distance determined under § 29.62 and the takeoff distance determined under § 29.61; (5) The landing data determined under § 29.81 and § 29.85; (6) The steady gradient of climb for each weight, altitude, and temperature for which takeoff data are to be scheduled, along the takeoff path determined in the flight conditions required in § 29.67(a)(1) and (a)(2): (i) In the flight conditions required in § 29.67(a)(1) between the end of the takeoff distance and the point at which the rotorcraft is 200 feet above the takeoff surface (or 200 feet above the lowest point of the takeoff profile for elevated heliports); (ii) In the flight conditions required in § 29.67(a)(2) between the points at which the rotorcraft is 200 and 1000 feet above the takeoff surface (or 200 and 1000 feet above the lowest point of the takeoff profile for elevated heliports); and (7

official document · source cfr-2024 · id 14:§ 29.1587