Previous Page Page 335 Next Page  
background image

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 

VerDate Mar<15>2010 

10:12 Mar 18, 2014

Jkt 232046

PO 00000

Frm 00336

Fmt 8010

Sfmt 8010

Y:\SGML\232046.XXX

232046

pmangrum on DSK3VPTVN1PROD with CFR

  Previous Page Page 335 Next Page