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14 CFR Ch. I (1–1–14 Edition)
§ 25.859
provisions is requested, the following
must be met for each cargo or baggage
compartment with those provisions:
(a) The detection system must pro-
vide a visual indication to the flight
crew within one minute after the start
of a fire.
(b) The system must be capable of de-
tecting a fire at a temperature signifi-
cantly below that at which the struc-
tural integrity of the airplane is sub-
stantially decreased.
(c) There must be means to allow the
crew to check in flight, the functioning
of each fire detector circuit.
(d) The effectiveness of the detection
system must be shown for all approved
operating configurations and condi-
tions.
[Amdt. 25–54, 45 FR 60173, Sept. 11, 1980, as
amended by Amdt. 25–93, 63 FR 8048, Feb. 17,
1998]
§ 25.859
Combustion heater fire pro-
tection.
(a)
Combustion heater fire zones. The
following combustion heater fire zones
must be protected from fire in accord-
ance with the applicable provisions of
§§ 25.1181 through 25.1191 and §§ 25.1195
through 25.1203;
(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 or vapors to enter this region.
(3) The part of the ventilating air
passage that surrounds the combustion
chamber. However, no fire extinguish-
ment is required in cabin ventilating
air passages.
(b)
Ventilating air ducts. Each ven-
tilating air duct passing through any
fire zone must be fireproof. In addi-
tion—
(1) Unless isolation is provided by
fireproof valves or by equally effective
means, the ventilating air duct down-
stream of each heater must be fireproof
for a distance great enough to ensure
that any fire originating in the heater
can be contained in the duct; and
(2) Each part of any ventilating duct
passing through any region having a
flammable fluid system must be con-
structed or isolated from that system
so that the malfunctioning of any com-
ponent of that system cannot intro-
duce flammable fluids or vapors into
the ventilating airstream.
(c)
Combustion air ducts. Each com-
bustion air duct must be fireproof for a
distance great enough to prevent dam-
age from backfiring or reverse flame
propagation. In addition—
(1) No combustion air duct may have
a common opening with the ventilating
airstream unless flames from backfires
or reverse burning cannot enter the
ventilating airstream under any oper-
ating condition, including reverse flow
or malfunctioning of the heater or its
associated components; and
(2) No combustion air duct may re-
strict the prompt relief of any backfire
that, if so restricted, could cause heat-
er failure.
(d)
Heater controls; general. Provision
must be made to prevent the hazardous
accumulation of water or ice on or in
any heater control component, control
system tubing, or safety control.
(e)
Heater safety controls. For each
combustion heater there must be the
following safety control means:
(1) Means independent of the compo-
nents provided for the normal contin-
uous control of air temperature, air-
flow, and fuel flow must be provided,
for each heater, to automatically shut
off the ignition and fuel supply to that
heater at a point remote from that
heater when any of the following oc-
curs:
(i) The heat exchanger temperature
exceeds safe limits.
(ii) The ventilating air temperature
exceeds safe limits.
(iii) The combustion airflow becomes
inadequate for safe operation.
(iv) The ventilating airflow becomes
inadequate for safe operation.
(2) The means of complying with
paragraph (e)(1) of this section for any
individual heater must—
(i) Be independent of components
serving any other heater whose heat
output is essential for safe operation;
and
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