775
Federal Aviation Administration, DOT
§ 36.501
FAA to be equivalent to the Chapter 14
noise levels required by the Inter-
national Civil Aviation Organization
(ICAO) in Annex 16, Volume 1, Aircraft
Noise, Seventh Edition, July 2014,
Amendment 11–B, applicable January 1,
2015.’’
[FAA Doc. No. FAA–2015–3782, Amdt. No. 36–
31, 82 FR 46129, Oct. 4, 2017]
Subpart C
[
Reserved
]
Subpart D—Noise Limits for Super-
sonic Transport Category Air-
planes
§ 36.301
Noise limits: Concorde.
(a)
General. For the Concorde air-
plane, compliance with this subpart
must be shown with noise levels meas-
ured and evaluated as prescribed in
Subpart B of this part, and dem-
onstrated at the measuring points pre-
scribed in appendix B of this part.
(b)
Noise limits. It must be shown, in
accordance with the provisions of this
part in effect on October 13, 1977, that
the noise levels of the airplane are re-
duced to the lowest levels that are eco-
nomically reasonable, technologically
practicable, and appropriate for the
Concorde type design.
[Amdt. 36–10, 43 FR 28420, June 29, 1978, as
amended by Amdt. 36–54, 67 FR 45212, July 8,
2002]
Subpart E
[
Reserved
]
Subpart F—Propeller Driven Small
Airplanes and Propeller-Driv-
en, Commuter Category Air-
planes
§ 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 cat-
egory is made on or after October 10,
1973; and propeller-driven, commuter
category airplanes for which applica-
tion for the issuance of a type certifi-
cate in the commuter category is made
on or after January 15, 1987.
(2) Propeller driven small airplanes
and propeller-driven, commuter cat-
egory airplanes for which application is
made for the original issuance of a
standard airworthiness certificate or
restricted category airworthiness cer-
tificate, and that have not had any
flight time before January 1, 1980 (re-
gardless of date of application).
(3) Airplanes in the primary cat-
egory:
(i) Except as provided in paragraph
(a)(3)(ii) of this section, for an airplane
for which application for a type certifi-
cate in the primary category is made,
and that was not previously certifi-
cated 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 airworthi-
ness certificate issued under this chap-
ter, (C) has not undergone an acous-
tical 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 conver-
sion to the primary category is made,
no further showing of compliance with
this part is required.
(b) For aircraft covered by this sub-
part 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 ap-
plicable limit set in Part D of appendix
F.
(c) For aircraft covered by this sub-
part 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 ap-
plicable limits set in Part D of appen-
dix 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]
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