Canadian Aviation Regulations (SOR/96-433)

Regulations are current to 2014-10-15 and last amended on 2014-05-29. Previous Versions

[602.147 to 602.149 reserved]

Division X — Noise Emission Levels for Subsonic Turbo-Jet Aeroplanes

Requirements

  •  (1) No person shall operate a subsonic turbo-jet aeroplane that has a maximum certificated take-off weight of 34 000 kg (74,956 pounds) or more to or from an aerodrome other than Gander International Airport unless the aeroplane meets the noise emission standards set out in Chapter 3 or 4 of Volume I, Aircraft Noise, of Annex 16 to the Convention.

  • (2) For the purpose of subsection (1), the following expressions, used in Annex 16 to the Convention, have the following meanings:

    • (a“aeroplane” has the same meaning as in subsection 101.01(1);

    • (b“maximum certificated take-off mass” has the same meaning as “maximum certificated take-off weight” in subsection 101.01(1); and

    • (c“subsonic jet” has the same meaning as “subsonic turbo-jet aeroplane” in subsection (1).

  • SOR/2008-277, s. 1;
  • SOR/2010-304, s. 3.

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]

 [Repealed, SOR/2008-277, s. 1]