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326
14 CFR Ch. I (1–1–14 Edition)
§ 23.1557
(2) Each emergency control must be
red and must be marked as to method
of operation. No control other than an
emergency control, or a control that
serves an emergency function in addi-
tion to its other functions, shall be this
color.
[Doc. No. 4080, 29 FR 17955, Dec. 18, 1964; 30
FR 258, Jan. 9, 1965, as amended by Amdt. 23–
21, 43 FR 2319, Jan. 16, 1978; Amdt. 23–50, 61
FR 5193, Feb. 9, 1996; Amdt. 23–62, 76 FR 75763,
Dec. 2, 2011]
§ 23.1557
Miscellaneous markings and
placards.
(a)
Baggage and cargo compartments,
and ballast location. Each baggage and
cargo compartment, and each ballast
location, must have a placard stating
any limitations on contents, including
weight, that are necessary under the
loading requirements.
(b)
Seats. If the maximum allowable
weight to be carried in a seat is less
than 170 pounds, a placard stating the
lesser weight must be permanently at-
tached to the seat structure.
(c)
Fuel, oil, and coolant filler open-
ings. The following apply:
(1) Fuel filler openings must be
marked at or near the filler cover
with—
(i) For reciprocating engine-powered
airplanes—
(A) The word ‘‘Avgas’’; and
(B) The minimum fuel grade.
(ii) For turbine engine-powered air-
planes—
(A) The words ‘‘Jet Fuel’’; and
(B) The permissible fuel designations,
or references to the Airplane Flight
Manual (AFM) for permissible fuel des-
ignations.
(iii) For pressure fueling systems, the
maximum permissible fueling supply
pressure and the maximum permissible
defueling pressure.
(2) Oil filler openings must be
marked at or near the filler cover with
the word ‘‘Oil’’ and the permissible oil
designations, or references to the Air-
plane Flight Manual (AFM) for permis-
sible oil designations.
(3) Coolant filler openings must be
marked at or near the filler cover with
the word ‘‘Coolant’’.
(d)
Emergency exit placards. Each
placard and operating control for each
emergency exit must be red. A placard
must be near each emergency exit con-
trol and must clearly indicate the loca-
tion of that exit and its method of op-
eration.
(e) The system voltage of each direct
current installation must be clearly
marked adjacent to its exernal power
connection.
[Doc. No. 4080, 29 FR 17955, Dec. 18, 1964; as
amended by Amdt. 23–21, 42 FR 15042, Mar. 17,
1977; Amdt. 23–23, 43 FR 50594, Oct. 30, 1978;
Amdt. 23–45, 58 FR 42166, Aug. 6, 1993; 73 FR
35063, June 20, 2008]
§ 23.1559
Operating limitations
placard.
(a) There must be a placard in clear
view of the pilot stating—
(1) That the airplane must be oper-
ated in accordance with the Airplane
Flight Manual; and
(2) The certification category of the
airplane to which the placards apply.
(b) For airplanes certificated in more
than one category, there must be a
placard in clear view of the pilot stat-
ing that other limitations are con-
tained in the Airplane Flight Manual.
(c) There must be a placard in clear
view of the pilot that specifies the kind
of operations to which the operation of
the airplane is limited or from which it
is prohibited under § 23.1525.
(d) The placard(s) required by this
section need not be lighted.
[Doc. No. 27807, 61 FR 5193, Feb. 9, 1996, as
amended by Amdt. 23–62, 76 FR 75763, Dec. 2,
2011]
§ 23.1561
Safety equipment.
(a) Safety equipment must be plainly
marked as to method of operation.
(b) Stowage provisions for required
safety equipment must be marked for
the benefit of occupants.
§ 23.1563
Airspeed placards.
There must be an airspeed placard in
clear view of the pilot and as close as
practicable to the airspeed indicator.
This placard must list—
(a) The operating maneuvering speed,
V
O
; and
(b) The maximum landing gear oper-
ating speed
V
LO
.
(c) For reciprocating multiengine-
powered airplanes of more than 6,000
pounds maximum weight, and turbine
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