Section 36.1583

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

(3) For rotorcraft, the noise level information must be one value for each
takeoff, flyover, and approach as defined and required by appendix H of
this part, or one value for flyover as
defined and required by appendix J of
this part, at the maximum takeoff
weight and configuration.
(b) If supplemental operational noise
level information is included in the approved portion of the Airplane Flight
Manual, it must be segregated, identified as information in addition to the
certificated noise levels, and clearly
distinguished from the information required under Section 36.1581(a).
(c) The following statement must be
furnished near the listed noise levels:

spaschal on DSK3GDR082PROD with CFR

No determination has been made by the Federal Aviation Administration that the noise
levels of this aircraft are or should be acceptable or unacceptable for operation at,
into, or out of, any airport.

(d) For transport category large airplanes and jet airplanes, for which the
weight used in meeting the takeoff or
landing noise requirements of this part
is less than the maximum weight established under the applicable airworthiness requirements, those lesser
weights must be furnished, as operating limitations in the operating limitations section of the Airplane Flight
Manual. Further, the maximum takeoff
weight must not exceed the takeoff
weight that is most critical from a
takeoff noise standpoint.
(e) For propeller driven small airplanes and for propeller-driven, commuter category airplanes for which the
weight used in meeting the flyover
noise requirements of this part is less
than the maximum weight by an
amount exceeding the amount of fuel
needed to conduct the test, that lesser
weight must be furnished, as an operating limitation, in the operating limitations section of an approved Airplane
Flight Manual, in approved manual
material, or on an approved placard.
(f) For primary, normal, transport,
and restricted category helicopters, if
the weight used in meeting the takeoff,
flyover, or approach noise requirements of appendix H of this part, or the
weight used in meeting the flyover
noise requirement of appendix J of this
part, is less than the certificated maximum takeoff weight established under

either Section 27.25(a) or Section 29.25(a) of this chapter, that lesser weight must be furnished as an operating limitation in
the operating limitations section of the
Rotorcraft Flight Manual, in FAA-approved manual material, or on an FAAapproved placard.
(g) Except as provided in paragraphs
(d), (e), and (f) of this section, no operating limitations are furnished under
this part.
[Doc. No. 13243, 40 FR 1035, Jan. 6, 1975]
EDITORIAL NOTE: For FEDERAL REGISTER citations affecting Section 36.1581, see the List of CFR
Sections Affected, which appears in the
Finding Aids section of the printed volume
and at www.govinfo.gov.

Section 36.1583 Noncomplying
agricultural
and fire fighting airplanes.
(a) This section applies to propellerdriven, small airplanes that - 
(1) Are designed for  - agricultural aircraft operations -  (as defined in Section 137.3
of this chapter, effective on January 1,
1966) or for dispensing fire fighting materials; and
(2) Have not been shown to comply
with the noise levels prescribed under
appendix F of this part - 
(i) For which application is made for
the original issue of a standard airworthiness certificate and that do not
have any flight time before January 1,
1980; or
(ii) For which application is made for
an acoustical change approval, for airplanes which have a standard airworthiness certificate after the change
in the type design, and that do not
have any flight time in the changed
configuration before January 1, 1980.
(b) For airplanes covered by this section an operating limitation reading as
follows must be furnished in the manner prescribed in Section 36.1581:
Noise abatement: This airplane has not
been shown to comply with the noise limits
in FAR Part 36 and must be operated in accordance with the noise operating limitation
prescribed under FAR Section 91.815.
[Amdt. 36-11, 45 FR 67066, Oct. 9, 1980. Redesignated by Amdt. 36-14, 53 FR 3540, Feb. 5,
1988; Amdt. 36-18, 54 FR 34330, Aug. 18, 1989]

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