Division 21.B.85 Designation of applicable environmental protection requirements and certification specifications for a type-certificate or restricted type-certificateF1F2

The F3CAA shall designate and notify to the applicant for a type-certificate or restricted type-certificate for an aircraft, for a supplemental type-certificate or for a major change to a type-certificate or to a supplemental type-certificate, the applicable noise requirements established in Annex 16 to the Chicago Convention, Volume I, Part II, Chapter 1 and:

1. 1..

   for subsonic jet aeroplanes, in Chapters 2, 3, 4 and 14;

2. 2..

   for propeller-driven aeroplanes in Chapters 3, 4, 5, 6, 10, and 14;

3. 3..

   for helicopters, in Chapters 8 and 11;

4. 4..

   for supersonic aeroplanes, in Chapter 12; and

5. 5..

   for tilt rotors, in Chapter 13.

The CAA shall designate and notify to the applicant referred to in point (a) the applicable emission requirements for preventions of intentional fuel venting for aircraft established in Annex 16 to the Chicago Convention, Volume II, Part II, Chapter 1 and 2.

The CAA shall designate and notify to the applicant referred to in point (a) the applicable smoke, gaseous and particulate matter engine emission requirements established in Annex 16 to the Chicago Convention, Volume II, Part III, Chapter 1 and

1. 1..

   for smoke and gaseous emissions of turbojet and turbofan engines intended for propulsion only at subsonic speeds, in Chapter 2;

2. 2..

   for smoke and gaseous emissions of turbojet and turbofan engines intended for propulsion at supersonic speeds, in Chapter 3;and

3. 3..

   for particulate matter emissions of turbojet and turbofan engines intended for propulsion only at subsonic speeds, in Chapter 4.

The CAA shall designate and notify to the applicant referred to in point (a) the applicable aeroplane CO ₂ emission requirements established in Annex 16 to the Chicago Convention, Volume III, Part II, Chapter 1 and

1. 1..

   for subsonic jet aeroplanes, in Chapter 2; and

2. 2..

   for subsonic propeller-driven aeroplanes, in Chapter 2.