371
Federal Aviation Administration, DOT
§ 25.1585
at which the airplane can be safely
flown with the landing gear extended.
(b)
Powerplant limitations. The fol-
lowing information must be furnished:
(1) Limitations required by § 25.1521
and § 25.1522.
(2) Explanation of the limitations,
when appropriate.
(3) Information necessary for mark-
ing the instruments required by
§§ 25.1549 through 25.1553.
(c)
Weight and loading distribution.
The weight and center of gravity limi-
tations established under § 25.1519 must
be furnished in the Airplane Flight
Manual. All of the following informa-
tion, including the weight distribution
limitations established under § 25.1519,
must be presented either in the Air-
plane Flight Manual or in a separate
weight and balance control and loading
document that is incorporated by ref-
erence in the Airplane Flight Manual:
(1) The condition of the airplane and
the items included in the empty weight
as defined in accordance with § 25.29.
(2) Loading instructions necessary to
ensure loading of the airplane within
the weight and center of gravity limits,
and to maintain the loading within
these limits in flight.
(3) If certification for more than one
center of gravity range is requested,
the appropriate limitations, with re-
gard to weight and loading procedures,
for each separate center of gravity
range.
(d)
Flight crew. The number and func-
tions of the minimum flight crew de-
termined under § 25.1523 must be fur-
nished.
(e)
Kinds of operation. The kinds of
operation approved under § 25.1525 must
be furnished.
(f)
Ambient air temperatures and oper-
ating altitudes. The extremes of the am-
bient air temperatures and operating
altitudes established under § 25.1527
must be furnished.
(g) [Reserved]
(h)
Additional operating limitations.
The operating limitations established
under § 25.1533 must be furnished.
(i)
Maneuvering flight load factors. The
positive maneuvering limit load fac-
tors for which the structure is proven,
described in terms of accelerations,
must be furnished.
[Doc. No. 5066, 29 FR 1891, Dec. 24, 1964, as
amended by Amdt. 25–38, 41 FR 55468, Dec. 20,
1976; Amdt. 25–42, 43 FR 2323, Jan. 16, 1978;
Amdt. 25–46, 43 FR 50598, Oct. 30, 1978; Amdt.
25–72, 55 FR 29787, July 20, 1990; Amdt. 25–105,
66 FR 34024, June 26, 2001; 75 FR 49818, Aug.
16, 2010]
§ 25.1585
Operating procedures.
(a) Operating procedures must be fur-
nished for—
(1) Normal procedures peculiar to the
particular type or model encountered
in connection with routine operations;
(2) Non-normal procedures for mal-
function cases and failure conditions
involving the use of special systems or
the alternative use of regular systems;
and
(3) Emergency procedures for foresee-
able but unusual situations in which
immediate and precise action by the
crew may be expected to substantially
reduce the risk of catastrophe.
(b) Information or procedures not di-
rectly related to airworthiness or not
under the control of the crew, must not
be included, nor must any procedure
that is accepted as basic airmanship.
(c) Information identifying each op-
erating condition in which the fuel sys-
tem independence prescribed in § 25.953
is necessary for safety must be fur-
nished, together with instructions for
placing the fuel system in a configura-
tion used to show compliance with that
section.
(d) The buffet onset envelopes, deter-
mined under § 25.251 must be furnished.
The buffet onset envelopes presented
may reflect the center of gravity at
which the airplane is normally loaded
during cruise if corrections for the ef-
fect of different center of gravity loca-
tions are furnished.
(e) Information must be furnished
that indicates that when the fuel quan-
tity indicator reads ‘‘zero’’ in level
flight, any fuel remaining in the fuel
tank cannot be used safely in flight.
(f) Information on the total quantity
of usable fuel for each fuel tank must
be furnished.
[Doc. No. 2000–8511, 66 FR 34024, June 26, 2001]
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