21.B.85 Designation of applicable environmental protection requirements for a type-certificate or restricted type-certificate

• Regulation (EU) 2021/1088 found in: Initial Airworthiness and Environmental Protection (No 748/2012) Part-21 Part-21L (Jul 2024)

21.B.85 Designation of applicable environmental protection requirements for a type-certificate or restricted type-certificate Regulation (EU) 2021/1088 (a)     The Agency shall designate and notify to the applicant the applicable environmental protection requirements for a type-certificate or restricted type-certificate for an aircraft or for a type certificate for an engine. The designation and notification shall contain: 1.       the applicable noise requirements established in: (i)      Annex 16 to the Chicago Convention, Volume I, Part II, Chapter 1 and: (A)     for subsonic jet aeroplanes, in Chapters 2, 3, 4 and 14; (B)     for propeller-driven aeroplanes, in Chapters 3, 4, 5, 6, 10, and 14; (C)     for helicopters, in Chapters 8 and 11; (D)     for supersonic aeroplanes, in Chapter 12; and (E)     for tilt rotors, in Chapter 13. (ii)     Annex 16 to the Chicago Convention, Volume I: (A)     Appendix 1 for aeroplanes for which Chapters 2 and 12 of Annex 16 to the Chicago Convention, Volume I, Part II are applicable; (B)     Appendix 2 for aeroplanes for which Chapters 3, 4, 5, 8, 13 and 14 of Annex 16 to the Chicago Convention, Volume I, Part II are applicable; (C)     Appendix 3 for aeroplanes for which Chapter 6 of Annex 16 to the Chicago Convention, Volume I, Part II is applicable; (D)     Appendix 4 for aeroplanes for which Chapter 11 of Annex 16 to the Chicago Convention, Volume I, Part II is applicable; and (E)     Appendix 6 for aeroplanes for which Chapter 10 of Annex 16 to the Chicago Convention, Volume I, Part II is applicable; 2.       the applicable emissions requirements for preventions of intentional fuel venting for aircraft established in Annex 16 to the Chicago Convention, Volume II, Part II, Chapters 1 and 2; 3.       the applicable smoke, gaseous and particulate matter engine emissions requirements established in: (i)      Annex 16 to the Chicago Convention, Volume II, Part III, Chapter 1 and: (A)     for smoke and gaseous emissions of turbojet and turbofan engines intended for propulsion only at subsonic speeds, in Chapter 2; (B)     for smoke and gaseous emissions of turbojet and turbofan engines intended for propulsion at supersonic speeds, in Chapter 3; and (C)     for particulate matter emissions of turbojet and turbofan engines intended for propulsion only at subsonic speeds, in Chapter 4; (ii)     Annex 16 to the Chicago Convention, Volume II: (A)     Appendix 1 for the measurement of reference pressure ratio; (B)     Appendix 2 for smoke emissions evaluation; (C)     Appendix 3 for instrumentation and measurement techniques for gaseous emissions; (D)     Appendix 4 for specifications for fuel to be used in aircraft turbine engine emissions testing; (E)     Appendix 5 for instrumentation and measurement techniques for gaseous emissions from afterburning gas turbine engines; (F)     Appendix 6 for compliance procedure for gaseous, smoke and particulate matter emissions; and (G)     Appendix 7 for instrumentation and measurement techniques for non-volatile particulate matter; 4.       the applicable aeroplane CO2 emissions requirements established in: (i)      Annex 16 to the Chicago Convention, Volume III, Part II, Chapter 1, and: (A)     for subsonic jet aeroplanes, in Chapter 2; and (B)     for subsonic propeller-driven aeroplanes, in Chapter 2;. (ii)     Annex 16 to the Chicago Convention, Volume III, Appendices 1 and 2, for aeroplanes for which Chapter 2 of Annex 16 to the Chicago Convention, Volume III, Part II is applicable; 5.       for engines, the applicable requirements in Annex 16 to the Chicago Convention, Volume II, Part IV and Appendix 8 concerning non-volatile particulate matter assessment for inventory and modelling purposes. (b)     (reserved).