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672
14 CFR Ch. I (1–1–14 Edition)
§ 27.831
(1) Consist of a movable window or
panel, or additional external door, pro-
viding an unobstructed opening that
will admit a 19-by 26-inch ellipse;
(2) Have simple and obvious methods
of opening, from the inside and from
the outside, which do not require ex-
ceptional effort;
(3) Be arranged and marked so as to
be readily located and opened even in
darkness; and
(4) Be reasonably protected from
jamming by fuselage deformation.
(c)
Tests. The proper functioning of
each emergency exit must be shown by
test.
(d)
Ditching emergency exits for pas-
sengers. If certification with ditching
provisions is requested, the markings
required by paragraph (b)(3) of this sec-
tion must be designed to remain visible
if the rotorcraft is capsized and the
cabin is submerged.
[Doc. No. 29247, 64 FR 45094, Aug. 18, 1999]
§ 27.831
Ventilation.
(a) The ventilating system for the
pilot and passenger compartments
must be designed to prevent the pres-
ence of excessive quantities of fuel
fumes and carbon monoxide.
(b) The concentration of carbon mon-
oxide may not exceed one part in 20,000
parts of air during forward flight or
hovering in still air. If the concentra-
tion exceeds this value under other
conditions, there must be suitable op-
erating restrictions.
§ 27.833
Heaters.
Each combustion heater must be ap-
proved.
[Amdt. 27–23, 53 FR 34210, Sept. 2, 1988]
F
IRE
P
ROTECTION
§ 27.853
Compartment interiors.
For each compartment to be used by
the crew or passengers—
(a) The materials must be at least
flame-resistant;
(b) [Reserved]
(c) If smoking is to be prohibited,
there must be a placard so stating, and
if smoking is to be allowed—
(1) There must be an adequate num-
ber of self-contained, removable ash-
trays; and
(2) Where the crew compartment is
separated from the passenger compart-
ment, there must be at least one illu-
minated sign (using either letters or
symbols) notifying all passengers when
smoking is prohibited. Signs which no-
tify when smoking is prohibited must—
(i) When illuminated, be legible to
each passenger seated in the passenger
cabin under all probable lighting condi-
tions; and
(ii) Be so constructed that the crew
can turn the illumination on and off.
[Amdt. 27–17, 45 FR 7755, Feb. 4, 1980, as
amended by Amdt. 27–37, 64 FR 45095, Aug. 18,
1999]
§ 27.855
Cargo and baggage compart-
ments.
(a) Each cargo and baggage compart-
ment must be constructed of, or lined
with, materials that are at least—
(1) Flame resistant, in the case of
compartments that are readily acces-
sible to a crewmember in flight; and
(2) Fire resistant, in the case of other
compartments.
(b) No compartment may contain any
controls, wiring, lines, equipment, or
accessories whose damage or failure
would affect safe operation, unless
those items are protected so that—
(1) They cannot be damaged by the
movement of cargo in the compart-
ment; and
(2) Their breakage or failure will not
create a fire hazard.
§ 27.859
Heating systems.
(a)
General. For each heating system
that involves the passage of cabin air
over, or close to, the exhaust manifold,
there must be means to prevent carbon
monoxide from entering any cabin or
pilot compartment.
(b)
Heat exchangers. Each heat ex-
changer must be—
(1) Of suitable materials;
(2) Adequately cooled under all con-
ditions; and
(3) Easily disassembled for inspec-
tion.
(c)
Combustion heater fire protection.
Except for heaters which incorporate
designs to prevent hazards in the event
of fuel leakage in the heater fuel sys-
tem, fire within the ventilating air pas-
sage, or any other heater malfunction,
each heater zone must incorporate the
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