[Code of Federal Regulations]

[Title 14, Volume 1]

[Revised as of January 1, 2006]

From the U.S. Government Printing Office via GPO Access

[CITE: 14CFR36.501]



[Page 820]

 

                     TITLE 14--AERONAUTICS AND SPACE

 

CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION

 

PART 36_NOISE STANDARDS: AIRCRAFT TYPE AND AIRWORTHINESS CERTIFICATION

--Table of Contents

 

    Subpart F_Propeller Driven Small Airplanes and Propeller-Driven, 

                       Commuter Category Airplanes

 

Sec. 36.501  Noise limits.





    (a) Compliance with this subpart must be shown for--

    (1) Propeller driven small airplanes for which application for the 

issuance of a new, amended, or supplemental type certificate in the 

normal, utility, acrobatic, transport, or restricted category is made on 

or after October 10, 1973; and propeller-driven, commuter category 

airplanes for which application for the issuance of a type certificate 

in the commuter category is made on or after January 15, 1987.

    (2) Propeller driven small airplanes and propeller-driven, commuter 

category airplanes for which application is made for the original 

issuance of a standard airworthiness certificate or restricted cate gory 

airworthiness certificate, and that have not had any flight time before 

January 1, 1980 (regardless of date of application).

    (3) Airplanes in the primary category:

    (i) Except as provided in paragraph (a)(3)(ii) of this section, for 

an airplane for which application for a type certificate in the primary 

category is made, and that was not previously certificated under 

appendix F of this part, compliance with appendix G of this part must be 

shown.

    (ii) For an airplane in the normal, utility or acrobatic category 

that (A) has a type certificate issued under this chapter, (B) has a 

standard airworthiness certificate issued under this chapter, (C) has 

not undergone an acoustical change from its type design, (D) has not 

previously been certificated under appendix F or G of this part, and (E) 

for which application for conversion to the primary category is made, no 

further showing of compliance with this part is required.

    (b) For aircraft covered by this subpart for which certification 

tests are completed before December 22, 1988, compliance must be shown 

with noise levels as measured and prescribed in Parts B and C of 

appendix F, or under approved equivalent procedures. It must be shown 

that the noise level of the airplane is no greater than the applicable 

limit set in Part D of appendix F.

    (c) For aircraft covered by this subpart for which certification 

tests are not completed before December 22, 1988, compliance must be 

shown with noise levels as measured and prescribed in Parts B and C of 

appendix G, or under approved equivalent procedures. It must be shown 

that the noise level of the airplane is no greater than the applicable 

limits set in Part D of appendix G.



[Doc. No. 13243, 40 FR 1034, Jan. 6, 1975, as amended by Amdt. 36-13, 52 

FR 1836, Jan. 15, 1987; Amdt. 36-16, 53 FR 47400, Nov. 22, 1988; Amdt. 

36-19, 57 FR 41369, Sept. 9, 1992]



Subpart G [Reserved]