Previous Page | Page 267 | Next Page |
258
14 CFR Ch. I (1–1–14 Edition)
§ 23.811
(3) Each required emergency exit, ex-
cept floor level exits, must be located
over the wing or, if not less than six
feet from the ground, must be provided
with an acceptable means to assist the
occupants to descend to the ground.
Emergency exits must be distributed as
uniformly as practical, taking into ac-
count passenger seating configuration.
(4) Unless the applicant has complied
with paragraph (d)(1) of this section,
there must be an emergency exit on
the side of the cabin opposite the pas-
senger entry door, provided that—
(i) For an airplane having a pas-
senger seating configuration of nine or
fewer, the emergency exit has a rectan-
gular opening measuring not less than
19 inches by 26 inches high with corner
radii not greater than one-third the
width of the exit, located over the
wing, with a step up inside the airplane
of not more than 29 inches and a step
down outside the airplane of not more
than 36 inches;
(ii) For an airplane having a pas-
senger seating configuration of 10 to 19
passengers, the emergency exit has a
rectangular opening measuring not less
than 20 inches wide by 36 inches high,
with corner radii not greater than one-
third the width of the exit, and with a
step up inside the airplane of not more
than 20 inches. If the exit is located
over the wing, the step down outside
the airplane may not exceed 27 inches;
and
(iii) The airplane complies with the
additional requirements of
§§ 23.561(b)(2)(iv), 23.803(b), 23.811(c),
23.812, 23.813(b), and 23.815.
(e) For multiengine airplanes, ditch-
ing emergency exits must be provided
in accordance with the following re-
quirements, unless the emergency exits
required by paragraph (a) or (d) of this
section already comply with them:
(1) One exit above the waterline on
each side of the airplane having the di-
mensions specified in paragraph (b) or
(d) of this section, as applicable; and
(2) If side exits cannot be above the
waterline, there must be a readily ac-
cessible overhead hatch emergency exit
that has a rectangular opening meas-
uring not less than 20 inches wide by 36
inches long, with corner radii not
greater than one-third the width of the
exit.
(3) In lieu of paragraph (e)(2) of this
section, if any side exit(s) cannot be
above the waterline, a device may be
placed at each of such exit(s) prior to
ditching. This device must slow the in-
flow of water when such exit(s) is
opened with the airplane ditched. For
commuter category airplanes, the clear
opening of such exit(s) must meet the
requirements defined in paragraph (d)
of this section.
[Doc. No. 4080, 29 FR 17955, Dec. 18, 1964, as
amended by Amdt. 23–7, 34 FR 13092, Aug. 13,
1969; Amdt. 23–10, 36 FR 2864, Feb. 11, 1971;
Amdt. 23–34, 52 FR 1831, Jan. 15, 1987; Amdt.
23–36, 53 FR 30814, Aug. 15, 1988; 53 FR 34194,
Sept. 2, 1988; Amdt. 23–46, 59 FR 25773, May
17, 1994; Amdt. 23–49, 61 FR 5167, Feb. 9, 1996;
Amdt. 23–62, 76 FR 75757, Dec. 2, 2011]
§ 23.811
Emergency exit marking.
(a) Each emergency exit and external
door in the passenger compartment
must be externally marked and readily
identifiable from outside the airplane
by—
(1) A conspicuous visual identifica-
tion scheme; and
(2) A permanent decal or placard on
or adjacent to the emergency exit
which shows the means of opening the
emergency exit, including any special
instructions, if applicable.
(b) In addition, for commuter cat-
egory airplanes, these exits and doors
must be internally marked with the
word ‘‘exit’’ by a sign which has white
letters 1 inch high on a red background
2 inches high, be self-illuminated or
independently, internally electrically
illuminated, and have a minimum
brightness of at least 160 micro-
lamberts. The color may be reversed if
the passenger compartment illumina-
tion is essentially the same.
(c) In addition, when certification to
the emergency exit provisions of
§ 23.807(d)(4) is requested, the following
apply:
(1) Each emergency exit, its means of
access, and its means of opening, must
be conspicuously marked;
(2) The identity and location of each
emergency exit must be recognizable
from a distance equal to the width of
the cabin;
(3) Means must be provided to assist
occupants in locating the emergency
exits in conditions of dense smoke;
VerDate Mar<15>2010
10:12 Mar 18, 2014
Jkt 232046
PO 00000
Frm 00268
Fmt 8010
Sfmt 8010
Y:\SGML\232046.XXX
232046
pmangrum on DSK3VPTVN1PROD with CFR
Previous Page | Page 267 | Next Page |