370
14 CFR Ch. I (1–1–24 Edition)
§ 25.1561
latched in the open position during
takeoff and landing.
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as
amended by Amdt. 25–32, 37 FR 3972, Feb. 24,
1972; Amdt. 25–38, 41 FR 55468, Dec. 20, 1976;
Amdt. 25–72, 55 FR 29786, July 20, 1990]
§ 25.1561
Safety equipment.
(a) Each safety equipment control to
be operated by the crew in emergency,
such as controls for automatic liferaft
releases, must be plainly marked as to
its method of operation.
(b) Each location, such as a locker or
compartment, that carries any fire ex-
tinguishing, signaling, or other life
saving equipment must be marked ac-
cordingly.
(c) Stowage provisions for required
emergency equipment must be con-
spicuously marked to identify the con-
tents and facilitate the easy removal of
the equipment.
(d) Each liferaft must have obviously
marked operating instructions.
(e) Approved survival equipment
must be marked for identification and
method of operation.
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as
amended by Amdt. 25–46, 43 FR 50598, Oct. 30,
1978]
§ 25.1563
Airspeed placard.
A placard showing the maximum air-
speeds for flap extension for the take-
off, approach, and landing positions
must be installed in clear view of each
pilot.
A
IRPLANE
F
LIGHT
M
ANUAL
§ 25.1581
General.
(a)
Furnishing information. An Air-
plane Flight Manual must be furnished
with each airplane, and it must contain
the following:
(1) Information required by §§ 25.1583
through 25.1587.
(2) Other information that is nec-
essary for safe operation because of de-
sign, operating, or handling character-
istics.
(3) Any limitation, procedure, or
other information established as a con-
dition of compliance with the applica-
ble noise standards of part 36 of this
chapter.
(b)
Approved information. Each part of
the manual listed in §§ 25.1583 through
25.1587, that is appropriate to the air-
plane, must be furnished, verified, and
approved, and must be segregated,
identified, and clearly distinguished
from each unapproved part of that
manual.
(c) [Reserved]
(d) Each Airplane Flight Manual
must include a table of contents if the
complexity of the manual indicates a
need for it.
[Amdt. 25–42, 43 FR 2323, Jan. 16, 1978, as
amended by Amdt. 25–72, 55 FR 29786, July 20,
1990]
§ 25.1583
Operating limitations.
(a)
Airspeed limitations. The following
airspeed limitations and any other air-
speed limitations necessary for safe op-
eration must be furnished:
(1) The maximum operating limit
speed
V
MO
/
M
MO
and a statement that
this speed limit may not be delib-
erately exceeded in any regime of
flight (climb, cruise, or descent) unless
a higher speed is authorized for flight
test or pilot training.
(2) If an airspeed limitation is based
upon compressibility effects, a state-
ment to this effect and information as
to any symptoms, the probable behav-
ior of the airplane, and the rec-
ommended recovery procedures.
(3) The maneuvering speed estab-
lished under § 25.1507 and statements,
as applicable to the particular design,
explaining that:
(i) Full application of pitch, roll, or
yaw controls should be confined to
speeds below the maneuvering speed;
and
(ii) Rapid and large alternating con-
trol inputs, especially in combination
with large changes in pitch, roll, or
yaw, and full control inputs in more
than one axis at the same time, should
be avoided as they may result in struc-
tural failures at any speed, including
below the maneuvering speed.
(4) The flap extended speed
V
FE
and
the pertinent flap positions and engine
powers.
(5) The landing gear operating speed
or speeds, and a statement explaining
the speeds as defined in § 25.1515(a).
(6) The landing gear extended speed
V
LE,
if greater than
V
LO,
and a state-
ment that this is the maximum speed
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