ADVOKS GLOBAL · KENYA
The Civil Aviation (Environmental Protection Aircraft Noise) Regulations, 2025
29. Applicability
Edition: 2026-03-03 · In force
29. Applicability
(1)This part shall be applicable to all propeller-driven aeroplanes, including their derived versions, of over 8 618 kg maximum certificated take-off mass for which either the application for a Type Certificate was submitted on or after 6 October 1977 and before 1 January 1985.(2)These Regulations, with the exception of Sections 2.1 and 2.4.2, shall be applicable to propeller-driven aeroplanes of over 8 618 kg for which the application for a Type Certificate was submitted before 6 October 1977 and which are either—(a)derived versions for which the application for certification of the change in type design was submitted on or after 6 October 1977; or(b)individual aeroplanes for which a certificate of airworthiness was first issued on or after 26 November 1981.(3)Notwithstanding regulation 29 (2) and 29(3), the Authority may recognize that the following situations for jet aeroplanes, and propeller-driven aeroplanes over 8 618 kg maximum certificated take-off mass on its registry do not require demonstration of compliance with the provisions of these Regulations—(a)gear down flight with one or more retractable landing gear down during the entire flight;(b)spare engine and nacelle carriage external to the skin of the aeroplane (and return of the pylon or other external mount); and(c)time-limited engine and/or nacelle changes, where the change in type design specifies that the aeroplane may not be operated for a period of more than 90 days unless compliance with these Regulations, is shown for that change in type design. This applies only to changes resulting from a required maintenance action.