This Part applies—
(a) | in respect of fuel venting, to turbine engine powered aircraft manufactured after 18 February 1982; |
(b) | in respect of engine emissions, to aircraft with— |
(i) | turbo-jet or turbofan engines intended for propulsion only at subsonic speeds; and |
(ii) | turbo-jet and turbofan engines intended for propulsion at supersonic speeds, of which the date of manufacture is 18 February 1982 or later; |
(c) | in respect of non-volatile particulate matter emissions, to aircraft with turbo-jet or turbofan engines intended for propulsion only at subsonic speeds, manufactured on or after 1 January 2020; |
(d) | to aeroplane CO2 emissions produced by— |
(i) | a subsonic jet aeroplane having an MTOM of greater than 5 700 kg for which an application for a type certificate was submitted not earlier than 1 January 2023; |
(ii) | a propeller-driven aeroplane, having an MTOM of greater than 8 618 kg, for which an application for a type certificate was submitted not earlier than 1 January 2020; |
(iii) | a derived version of non-CO2-certified subsonic jet aeroplane having an MCTOM of greater than 5 700 kg for which an application for certification of a change in type design was submitted not earlier than 1 January 2023: |
(iv) | a derived version of non-CO2 certified propeller-driven aeroplane having an MCTOM of greater than 8 618 kg for which an application for certification of a change in type design was submitted not earlier than 1 January 2023; |
(v) | an individual non-CO2-certified subsonic jet aeroplane having an MCTOM of greater than 5 700 kg first issued with a certificate of airworthiness not earlier than 1 January 2028; and |
(vi) | an individual non-CO2-certified propeller-driven aeroplane having an MCTOM of greater than 8 618 kg first issued with a certificate of airworthiness not earlier than 1 January 2028. |
[Regulation 34.01.1 substituted by regulation 6(b) of Notice No. R. 3169, GG 48228, dated 17 March 2023 (Twenty-Fifth Amendment of the Civil Aviation Regulations, 2023)]