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14 CFR Ch. I (1–1–14 Edition)
§ 23.855
compartments unless adequately
shielded, isolated, or otherwise pro-
tected so that any breakage or failure
of such an item would not create a haz-
ard.
(f) Airplane materials located on the
cabin side of the firewall must be self-
extinguishing or be located at such a
distance from the firewall, or otherwise
protected, so that ignition will not
occur if the firewall is subjected to a
flame temperature of not less than
2,000 degrees F for 15 minutes. For self-
extinguishing materials (except elec-
trical wire and cable insulation and
small parts that the Administrator
finds would not contribute signifi-
cantly to the propagation of a fire), a
vertifical self-extinguishing test must
be conducted in accordance with appen-
dix F of this part or an equivalent
method approved by the Adminis-
trator. The average burn length of the
material may not exceed 6 inches and
the average flame time after removal
of the flame source may not exceed 15
seconds. Drippings from the material
test specimen may not continue to
flame for more than an average of 3
seconds after falling.
[Amdt. 23–14, 23 FR 31822, Nov. 19, 1973, as
amended by Amdt. 23–23, 43 FR 50593, Oct. 30,
1978; Amdt. 23–25, 45 FR 7755, Feb. 4, 1980;
Amdt. 23–34, 52 FR 1831, Jan. 15, 1987; Amdt.
23–62, 76 FR 75759, Dec. 2, 2011]
§ 23.855
Cargo and baggage compart-
ment fire protection.
(a) Sources of heat within each cargo
and baggage compartment that are ca-
pable of igniting the compartment con-
tents must be shielded and insulated to
prevent such ignition.
(b) Each cargo and baggage compart-
ment must be constructed of materials
that meet the appropriate provisions of
§ 23.853(d)(3).
(c) In addition, for commuter cat-
egory airplanes, each cargo and bag-
gage compartment must:
(1) Be located where the presence of a
fire would be easily discovered by the
pilots when seated at their duty sta-
tion, or it must be equipped with a
smoke or fire detector system to give a
warning at the pilots’ station, and pro-
vide sufficient access to enable a pilot
to effectively reach any part of the
compartment with the contents of a
hand held fire extinguisher, or
(2) Be equipped with a smoke or fire
detector system to give a warning at
the pilots’ station and have ceiling and
sidewall liners and floor panels con-
structed of materials that have been
subjected to and meet the 45 degree
angle test of appendix F of this part.
The flame may not penetrate (pass
through) the material during applica-
tion of the flame or subsequent to its
removal. The average flame time after
removal of the flame source may not
exceed 15 seconds, and the average glow
time may not exceed 10 seconds. The
compartment must be constructed to
provide fire protection that is not less
than that required of its individual
panels; or
(3) Be constructed and sealed to con-
tain any fire within the compartment.
[Doc. No. 27806, 61 FR 5167, Feb. 9, 1996]
§ 23.856
Thermal/acoustic insulation
materials.
Thermal/acoustic insulation material
installed in the fuselage must meet the
flame propagation test requirements of
part II of Appendix F to this part, or
other approved equivalent test require-
ments. This requirement does not
apply to ‘‘small parts,’’ as defined in
§ 23.853(d)(3)(v).
[Amdt. 23–62, 76 FR 75759, Dec. 2, 2011]
§ 23.859
Combustion heater fire pro-
tection.
(a)
Combustion heater fire regions. The
following combustion heater fire re-
gions must be protected from fire in ac-
cordance with the applicable provisions
of §§ 23.1182 through 23.1191 and 23.1203:
(1) The region surrounding the heat-
er, if this region contains any flam-
mable fluid system components (ex-
cluding the heater fuel system) that
could—
(i) Be damaged by heater malfunc-
tioning; or
(ii) Allow flammable fluids or vapors
to reach the heater in case of leakage.
(2) The region surrounding the heat-
er, if the heater fuel system has fit-
tings that, if they leaked, would allow
fuel vapor to enter this region.
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