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267
Federal Aviation Administration, DOT
§ 23.859
(3) The part of the ventilating air
passage that surrounds the combustion
chamber.
(b)
Ventilating air ducts. Each ven-
tilating air duct passing through any
fire region 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. (1) Each
combustion heater must have the fol-
lowing safety controls:
(i) Means independent of the compo-
nents for the normal continuous con-
trol of air temperature, airflow, and
fuel flow must be provided to auto-
matically shut off the ignition and fuel
supply to that heater at a point remote
from that heater when any of the fol-
lowing occurs:
(A) The heater exchanger tempera-
ture exceeds safe limits.
(B) The ventilating air temperature
exceeds safe limits.
(C) The combustion airflow becomes
inadequate for safe operation.
(D) The ventilating airflow becomes
inadequate for safe operation.
(ii) Means to warn the crew when any
heater whose heat output is essential
for safe operation has been shut off by
the automatic means prescribed in
paragraph (e)(1)(i) of this section.
(2) The means for complying with
paragraph (e)(1)(i) of this section for
any individual heater must—
(i) Be independent of components
serving any other heater whose heat
output is essential for safe operations;
and
(ii) Keep the heater off until re-
started by the crew.
(f)
Air intakes. Each combustion and
ventilating air intake must be located
so that no flammable fluids or vapors
can enter the heater system under any
operating condition—
(1) During normal operation; or
(2) As a result of the malfunctioning
of any other component.
(g)
Heater exhaust. Heater exhaust
systems must meet the provisions of
§§ 23.1121 and 23.1123. In addition, there
must be provisions in the design of the
heater exhaust system to safely expel
the products of combustion to prevent
the occurrence of—
(1) Fuel leakage from the exhaust to
surrounding compartments;
(2) Exhaust gas impingement on sur-
rounding equipment or structure;
(3) Ignition of flammable fluids by
the exhaust, if the exhaust is in a com-
partment containing flammable fluid
lines; and
(4) Restrictions in the exhaust sys-
tem to relieve backfires that, if so re-
stricted, could cause heater failure.
(h)
Heater fuel systems. Each heater
fuel system must meet each power-
plant fuel system requirement affect-
ing safe heater operation. Each heater
fuel system component within the ven-
tilating airstream must be protected
by shrouds so that no leakage from
those components can enter the ven-
tilating airstream.
(i)
Drains. There must be means to
safely drain fuel that might accumu-
late within the combustion chamber or
the heater exchanger. In addition—
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