General.

CFR · 2024-01-01 · US · Title 14

(a) (1) Limit ground loads obtained under this subpart are considered to be external forces applied to the airplane structure; and (2) In each specified ground load condition, the external loads must be placed in equilibrium with the linear and angular inertia loads in a rational or conservative manner. (b) (1) The lateral displacement of the c.g. results from random passenger or cargo disposition within the fuselage or from random unsymmetrical fuel loading or fuel usage; and (2) Appropriate loading instructions for random disposable loads are included under the provisions of § 25.1583(c)(2) to ensure that the lateral (c)

official document · source cfr-2024 · id 14:§ 25.471