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14 CFR Ch. I (1–1–19 Edition)
§ 25.811
(b) The identity and location of each
passenger emergency exit must be rec-
ognizable from a distance equal to the
width of the cabin.
(c) Means must be provided to assist
the occupants in locating the exits in
conditions of dense smoke.
(d) The location of each passenger
emergency exit must be indicated by a
sign visible to occupants approaching
along the main passenger aisle (or
aisles). There must be—
(1) A passenger emergency exit loca-
tor sign above the aisle (or aisles) near
each passenger emergency exit, or at
another overhead location if it is more
practical because of low headroom, ex-
cept that one sign may serve more
than one exit if each exit can be seen
readily from the sign;
(2) A passenger emergency exit mark-
ing sign next to each passenger emer-
gency exit, except that one sign may
serve two such exits if they both can be
seen readily from the sign; and
(3) A sign on each bulkhead or divider
that prevents fore and aft vision along
the passenger cabin to indicate emer-
gency exits beyond and obscured by the
bulkhead or divider, except that if this
is not possible the sign may be placed
at another appropriate location.
(e) The location of the operating han-
dle and instructions for opening exits
from the inside of the airplane must be
shown in the following manner:
(1) Each passenger emergency exit
must have, on or near the exit, a mark-
ing that is readable from a distance of
30 inches.
(2) Each Type A, Type B, Type C or
Type I passenger emergency exit oper-
ating handle must—
(i) Be self-illuminated with an initial
brightness of at least 160 micro-
lamberts; or
(ii) Be conspicuously located and well
illuminated by the emergency lighting
even in conditions of occupant crowd-
ing at the exit.
(3) [Reserved]
(4) Each Type A, Type B, Type C,
Type I, or Type II passenger emergency
exit with a locking mechanism re-
leased by rotary motion of the handle
must be marked—
(i) With a red arrow, with a shaft at
least three-fourths of an inch wide and
a head twice the width of the shaft, ex-
tending along at least 70 degrees of arc
at a radius approximately equal to
three-fourths of the handle length.
(ii) So that the centerline of the exit
handle is within
±
1 inch of the pro-
jected point of the arrow when the han-
dle has reached full travel and has re-
leased the locking mechanism, and
(iii) With the word ‘‘open’’ in red let-
ters 1 inch high, placed horizontally
near the head of the arrow.
(f) Each emergency exit that is re-
quired to be openable from the outside,
and its means of opening, must be
marked on the outside of the airplane.
In addition, the following apply:
(1) The outside marking for each pas-
senger emergency exit in the side of
the fuselage must include a 2-inch col-
ored band outlining the exit.
(2) Each outside marking including
the band, must have color contrast to
be readily distinguishable from the sur-
rounding fuselage surface. The contrast
must be such that if the reflectance of
the darker color is 15 percent or less,
the reflectance of the lighter color
must be at least 45 percent. ‘‘Reflec-
tance’’ is the ratio of the luminous flux
reflected by a body to the luminous
flux it receives. When the reflectance
of the darker color is greater than 15
percent, at least a 30-percent difference
between its reflectance and the reflec-
tance of the lighter color must be pro-
vided.
(3) In the case of exists other than
those in the side of the fuselage, such
as ventral or tailcone exists, the exter-
nal means of opening, including in-
structions if applicable, must be con-
spicuously marked in red, or bright
chrome yellow if the background color
is such that red is inconspicuous. When
the opening means is located on only
one side of the fuselage, a conspicuous
marking to that effect must be pro-
vided on the other side.
(g) Each sign required by paragraph
(d) of this section may use the word
‘‘exit’’ in its legend in place of the
term ‘‘emergency exit’’.
[Amdt. 25–15, 32 FR 13264, Sept. 20, 1967, as
amended by Amdt. 25–32, 37 FR 3970, Feb. 24,
1972; Amdt. 25–46, 43 FR 50597, Oct. 30, 1978; 43
FR 52495, Nov. 13, 1978; Amdt. 25–79, 58 FR
45229, Aug. 26, 1993; Amdt. 25–88, 61 FR 57958,
Nov. 8, 1996]
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