36.1 Applicability and definitions.
top (a) This part prescribes noise standards for the issue of the following certificates: (1) Type certificates, and changes to those certificates, and standard airworthiness certificates, for subsonic transport category large airplanes, and for subsonic jet airplanes regardless of category. (2) Type certificates and changes to those certificates, standard airworthiness certificates, and restricted category airworthiness certificates, for propeller-driven, small airplanes, and for propeller-driven, commuter category airplanes except those airplanes that are designed for agricultural aircraft operations (as defined in 137.3 of this chapter, as effective on January 1, 1966) or for dispersing fire fighting materials to which 36.1583 of this part does not apply. (3) A type certificate and changes to that certificate, and standard airworthiness certificates, for Concorde airplanes. (4) Type certificates, and changes to those certificates, for helicopters except those helicopters that are designated exclusively for argicultural aircraft operations (as defined in 137.3 of this chapter, as effective on January 1, 1966), for dispensing fire fighting materials, or for carrying external loads (as defined in 133.1(b) of this chapter, as effective on December 20, 1976). (b) Each person who applies under Part 21 of this chapter for a type of airworthiness certificate specified in this part must show compliance with the applicable requirements of this part, in addition to the applicable airworthiness requirements of this chapter. (c) Each person who applies under Part 21 of this chapter for approval of an acoustical change described in 21.93(b) of this chapter must show that the aircraft complies with the applicable provisions of 36.7, 36.9, or 36.11 of this part in addition to the applicable airworthiness requirements of this chapter. (d) Each person who applies for the original issue of a standard airworthiness certificate for a transport category large airplane or for a jet airplane under 21.183 must, regardless of date of application, show compliance with the following provisions of this part (including appendix B): (1) The provisions of this part in effect on December 1, 1969, for subsonic airplanes that have not had any flight time before (i) December 1, 1973, for airplanes with maximum weights greater than 75,000 pounds, except for airplanes that are powered by Pratt & Whitney Turbo Wasp JT3D series engines; (ii) December 31, 1974, for airplanes with maximum weights greater than 75,000 pounds and that are powered by Pratt & Whitney Turbo Wasp JT3D series engines; and (iii) December 31, 1974, for airplanes with maximum weights of 75,000 pounds and less. (2) The provisions of this part in effect on October 13, 1977, including the stage 2 noise limits, for Concorde airplanes that have not had flight time before January 1, 1980. (e) Each person who applies for the original issue of a standard airworthiness certificate under 21.183, or