764
14 CFR Ch. I (1–1–19 Edition)
§ 36.1
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.
A
PPENDIX
A
TO
P
ART
36—A
IRCRAFT
N
OISE
M
EASUREMENT
AND
E
VALUATION
U
NDER
§ 36.101
A
PPENDIX
B
TO
P
ART
36—N
OISE
L
EVELS FOR
T
RANSPORT
C
ATEGORY
AND
J
ET
A
IR
-
PLANES
U
NDER
§ 36.103
A
PPENDIXES
C–E
TO
P
ART
36 [R
ESERVED
]
A
PPENDIX
F
TO
P
ART
36—F
LYOVER
N
OISE
R
E
-
QUIREMENTS
FOR
P
ROPELLER
-D
RIVEN
S
MALL
A
IRPLANE AND
P
ROPELLER
-D
RIVEN
,
C
OMMUTER
C
ATEGORY
A
IRPLANE
C
ERTIFI
-
CATION
T
ESTS
P
RIOR TO
D
ECEMBER
22, 1988
A
PPENDIX
G
TO
P
ART
36—T
AKEOFF
N
OISE
R
E
-
QUIREMENTS
FOR
P
ROPELLER
-D
RIVEN
S
MALL
A
IRPLANE AND
P
ROPELLER
-D
RIVEN
,
C
OMMUTER
C
ATEGORY
A
IRPLANE
C
ERTIFI
-
CATION
T
ESTS ON OR
A
FTER
D
ECEMBER
22,
1988
A
PPENDIX
H
TO
P
ART
36—N
OISE
R
EQUIRE
-
MENTS FOR
H
ELICOPTERS
U
NDER
S
UBPART
H
A
PPENDIX
I
TO
P
ART
36 [R
ESERVED
]
A
PPENDIX
J
TO
P
ART
36—A
LTERNATIVE
N
OISE
C
ERTIFICATION
P
ROCEDURE
F
OR
H
ELI
-
COPTERS
U
NDER
S
UBPART
H H
AVING
A
M
AXIMUM
C
ERTIFICATED
T
AKEOFF
W
EIGHT
O
F
N
OT
M
ORE
T
HAN
7,000 P
OUNDS
A
PPENDIX
K
TO
P
ART
36—N
OISE
R
EQUIRE
-
MENTS FOR
T
ILTROTORS
U
NDER
S
UBPART
K
A
UTHORITY
: 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.
S
OURCE
: Docket No. 9337, 34 FR 18364, Nov.
18, 1969, unless otherwise noted.
Subpart A—General
§ 36.1
Applicability and definitions.
(a) This part prescribes noise stand-
ards for the issue of the following cer-
tificates:
(1) Type certificates, and changes to
those certificates, and standard air-
worthiness certificates, for subsonic
transport category large airplanes, and
for subsonic jet airplanes regardless of
category.
(2) Type certificates and changes to
those certificates, standard airworthi-
ness certificates, and restricted cat-
egory airworthiness certificates, for
propeller-driven, small airplanes, and
for propeller-driven, commuter cat-
egory airplanes except those airplanes
that are designed for ‘‘agricultural air-
craft 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 air-
worthiness certificates, for Concorde
airplanes.
(4) Type certificates, and changes to
those certificates, for helicopters ex-
cept those helicopters that are des-
ignated 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 ex-
ternal loads (as defined in § 133.1(b) of
this chapter, as effective on December
20, 1976).
(5) Type certificates, changes to
those certificates, and standard air-
worthiness certificates, for tiltrotors.
(b) Each person who applies under
Part 21 of this chapter for a type of air-
worthiness certificate specified in this
part must show compliance with the
applicable requirements of this part, in
addition to the applicable airworthi-
ness 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 applica-
ble provisions of §§ 36.7, 36.9, 36.11 or
36.13 of this part in addition to the ap-
plicable airworthiness requirements of
this chapter.
(d) Each person who applies for the
original issue of a standard airworthi-
ness certificate for a transport cat-
egory large airplane or for a jet air-
plane 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 ef-
fect 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
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