Sec. 36.1581 - Manuals, markings, and placards.
(a) If an Airplane Flight Manual or Rotorcraft Flight Manual is
approved, the approved portion of the Airplane Flight Manual or Rotorcraft
Flight Manual must contain the following information, in addition to that
specified under §36.1583 of this part. If an Airplane Flight Manual or
Rotorcraft Flight Manual is not approved, the procedures and information
must be furnished in any combination of approved manual material,
markings, and placards.
(1) For transport category large airplanes and jet airplanes, the noise
level information must be one value for each flyover, lateral, and
approach as defined and required by appendix B of this part, along with
the maximum takeoff weight, maximum landing weight, and configuration.
(2) For propeller driven small airplanes the noise level information
must be one value for flyover as defined and required by appendix F of
this part, along with 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 §36.1581(a).
(c) The following statement must be furnished near the listed noise
levels:
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
§27.25(a) or §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
FAA-approved placard.
(g) Except as provided in paragraphs (d), (e), and (f) of this section,
no operating limitations are furnished under this part.
[Doc. 13243, 40 FR 1035, Jan. 6, 1975 as amended by Amdt. 36-10,
43 FR 28420, June 29, 1978; Amdt. 36-11, 45 FR 67066, Oct. 9, 1980; Amdt.
36-13, 52 FR 1836, Jan. 15, 1987. Redesignated and amended by Amdt. 36-14,
53 FR 3540, Feb. 5, 1988; 53 FR 7728, Mar. 10, 1988; Amdt. 36-15, 53 FR
16366, May 6, 1988; 53 FR 18950, May 25, 1988; Amdt. 36-20, 57 FR 42855,
Sept. 16, 1992; Amdt. 36-54, 67 FR 45212, July 8, 2002]