Marking of products.

CFR · 2024-01-01 · US · Title 14

(a) (1) Includes the information specified in § 45.13 using an approved method of fireproof marking; (2) Must be secured in such a manner that it will not likely be defaced or removed during normal service, or lost or destroyed in an accident; and (3) Except as provided in paragraphs (d) through (h) of this section, must be secured to the aircraft fuselage exterior so that it is legible to a person on the ground, and must be either adjacent to and aft of the rear-most entrance door or on the fuselage surface near the tail surfaces. (b) (1) Must include the information specified in § 45.13 using an approved method of fireproof marking; (2) Must be affixed to the engine at an accessible location; and (3) Must be secured in such a manner that it will not likely be defaced or removed during normal service, or lost or destroyed in an accident. (c) (1) Be placed on a non-critical surface; (2) Contain the information specified in § 45.13; (3) Not likely be defaced or removed during normal service; and (4) Not likely be lost or destroyed in an accident. (d) (e) (1) Legible to a person on the ground, (2) Located either adjacent to and aft of the rear-most entrance door or on the fuselage near the tail surfaces, and (3) Displayed in such a manner that they are not likely to be defaced or removed during normal service. (f) For powered parachutes and weight-shift-control aircraft, the identification plate required by paragraph (a) of this section must be secured to the exterior of the ai

official document · source cfr-2024 · id 14:§ 45.11