Section 36.1

14 CFR Ch. I (1-1-19 Edition)

Subpart O - Documentation, Operating
Limitations and Information
36.1501 Procedures, noise levels and other
information.
36.1581 Manuals, markings, and placards.
36.1583 Noncomplying agricultural and fire
fighting airplanes.
APPENDIX A TO PART 36 - AIRCRAFT NOISE
MEASUREMENT AND EVALUATION UNDER
Section 36.101
APPENDIX B TO PART 36 - NOISE LEVELS FOR
TRANSPORT CATEGORY AND JET AIRPLANES UNDER Section 36.103
APPENDIXES C-E TO PART 36 [RESERVED]
APPENDIX F TO PART 36 - FLYOVER NOISE REQUIREMENTS
FOR
PROPELLER-DRIVEN
SMALL AIRPLANE AND PROPELLER-DRIVEN,
COMMUTER CATEGORY AIRPLANE CERTIFICATION TESTS PRIOR TO DECEMBER 22, 1988
APPENDIX G TO PART 36 - TAKEOFF NOISE REQUIREMENTS
FOR
PROPELLER-DRIVEN
SMALL AIRPLANE AND PROPELLER-DRIVEN,
COMMUTER CATEGORY AIRPLANE CERTIFICATION TESTS ON OR AFTER DECEMBER 22,
1988
APPENDIX H TO PART 36 - NOISE REQUIREMENTS FOR HELICOPTERS UNDER SUBPART
H
APPENDIX I TO PART 36 [RESERVED]
APPENDIX J TO PART 36 - ALTERNATIVE NOISE
CERTIFICATION PROCEDURE FOR HELICOPTERS UNDER SUBPART H HAVING A
MAXIMUM CERTIFICATED TAKEOFF WEIGHT
OF NOT MORE THAN 7,000 POUNDS
APPENDIX K TO PART 36 - NOISE REQUIREMENTS FOR TILTROTORS UNDER SUBPART K
AUTHORITY: 42 U.S.C. 4321 et seq.; 49 U.S.C.
106(g), 40113, 44701-44702, 44704, 44715; sec. 305,
Pub. L. 96-193, 94 Stat. 50, 57; E.O. 11514, 35
FR 4247, 3 CFR, 1966-1970 Comp., p. 902.
SOURCE: Docket No. 9337, 34 FR 18364, Nov.
18, 1969, unless otherwise noted.

spaschal on DSK3GDR082PROD with CFR

Subpart A - General
Section 36.1 Applicability and definitions.
(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 Section 137.3
of this chapter, as effective on January
1, 1966) or for dispersing fire fighting
materials to which Section 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
Section 137.3 of this chapter, as effective on
January 1, 1966), for dispensing fire
fighting materials, or for carrying external loads (as defined in Section 133.1(b) of
this chapter, as effective on December
20, 1976).
(5) Type certificates, changes to
those certificates, and standard airworthiness certificates, for tiltrotors.
(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
Section 21.93(b) of this chapter must show that
the aircraft complies with the applicable provisions of SectionSection 36.7, 36.9, 36.11 or
36.13 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 Section 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 Section Whitney Turbo
Wasp JT3D series engines;
(ii) December 31, 1974, for airplanes
with maximum weights greater than

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