Operating limitations.

CFR · 2024-01-01 · US · Title 14

(a) (1) The maximum operating limit speed (2) If an airspeed limitation is based upon compressibility effects, a statement to this effect and information as to any symptoms, the probable behavior of the airplane, and the recommended recovery procedures. (3) The maneuvering speed established under § 25.1507 and statements, as applicable to the particular design, explaining that: (i) Full application of pitch, roll, or yaw controls should be confined to speeds below the maneuvering speed; and (ii) Rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw, and full control inputs in more than one axis at the same time, should be avoided as they may result in structural failures at any speed, including below the maneuvering speed. (4) The flap extended speed (5) The landing gear operating speed or speeds, and a statement explaining the speeds as defined in § 25.1515(a). (6) The landing gear extended speed (b) (1) Limitations required by § 25.1521 and § 25.1522. (2) Explanation of the limitations, when appropriate. (3) Information necessary for marking the instruments required by §§ 25.1549 through 25.1553. (c) (1) The condition of the airplane and the items included in the empty weight as defined in accordance with § 25.29. (2) Loading instructions necessary to ensure loading of the airplane within the weight and center of gravity limits, and to maintain the loading within these limits in flight. (3) If certification for more

official document · source cfr-2024 · id 14:§ 25.1583