764
14 CFR Ch. I (1–1–14 Edition)
§§ 91.536–91.599
(d) No operator may permit an air-
craft to move on the surface, take off,
or land unless each movie screen that
extends into the aisle is stowed.
(e) Each passenger shall comply with
instructions given by a crewmember
with regard to compliance with this
section.
[Doc. No. 26142, 57 FR 42672, Sept. 15, 1992]
§§ 91.536–91.599
[Reserved]
Subpart G—Additional Equipment
and Operating Requirements
for Large and Transport Cat-
egory Aircraft
S
OURCE
: Docket No. 18334, 54 FR 34318, Aug.
18, 1989, unless otherwise noted.
§ 91.601
Applicability.
This subpart applies to operation of
large and transport category U.S.-reg-
istered civil aircraft.
§ 91.603
Aural speed warning device.
No person may operate a transport
category airplane in air commerce un-
less that airplane is equipped with an
aural speed warning device that com-
plies with § 25.1303(c)(1).
§ 91.605
Transport category civil air-
plane weight limitations.
(a) No person may take off any trans-
port category airplane (other than a
turbine-engine-powered airplane cer-
tificated after September 30, 1958) un-
less—
(1) The takeoff weight does not ex-
ceed the authorized maximum takeoff
weight for the elevation of the airport
of takeoff;
(2) The elevation of the airport of
takeoff is within the altitude range for
which maximum takeoff weights have
been determined;
(3) Normal consumption of fuel and
oil in flight to the airport of intended
landing will leave a weight on arrival
not in excess of the authorized max-
imum landing weight for the elevation
of that airport; and
(4) The elevations of the airport of in-
tended landing and of all specified al-
ternate airports are within the altitude
range for which the maximum landing
weights have been determined.
(b) No person may operate a turbine-
engine-powered transport category air-
plane certificated after September 30,
1958, contrary to the Airplane Flight
Manual, or take off that airplane un-
less—
(1) The takeoff weight does not ex-
ceed the takeoff weight specified in the
Airplane Flight Manual for the ele-
vation of the airport and for the ambi-
ent temperature existing at the time of
takeoff;
(2) Normal consumption of fuel and
oil in flight to the airport of intended
landing and to the alternate airports
will leave a weight on arrival not in ex-
cess of the landing weight specified in
the Airplane Flight Manual for the ele-
vation of each of the airports involved
and for the ambient temperatures ex-
pected at the time of landing;
(3) The takeoff weight does not ex-
ceed the weight shown in the Airplane
Flight Manual to correspond with the
minimum distances required for take-
off, considering the elevation of the
airport, the runway to be used, the ef-
fective runway gradient, the ambient
temperature and wind component at
the time of takeoff, and, if operating
limitations exist for the minimum dis-
tances required for takeoff from wet
runways, the runway surface condition
(dry or wet). Wet runway distances as-
sociated with grooved or porous fric-
tion course runways, if provided in the
Airplane Flight Manual, may be used
only for runways that are grooved or
treated with a porous friction course
(PFC) overlay, and that the operator
determines are designed, constructed,
and maintained in a manner acceptable
to the Administrator.
(4) Where the takeoff distance in-
cludes a clearway, the clearway dis-
tance is not greater than one-half of—
(i) The takeoff run, in the case of air-
planes certificated after September 30,
1958, and before August 30, 1959; or
(ii) The runway length, in the case of
airplanes certificated after August 29,
1959.
(c) No person may take off a turbine-
engine-powered transport category air-
plane certificated after August 29, 1959,
unless, in addition to the requirements
of paragraph (b) of this section—
(1) The accelerate-stop distance is no
greater than the length of the runway
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