307
Federal Aviation Administration, DOT
§ 25.863
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
(ii) Keep the heater off until re-
started by the crew.
(3) There must be means to warn the
crew when any heater whose heat out-
put is essential for safe operation has
been shut off by the automatic means
prescribed in paragraph (e)(1) of this
section.
(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
§§ 25.1121 and 25.1123. 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) Restriction by the exhaust of the
prompt relief of 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 heat exchanger. In addition—
(1) Each part of any drain that oper-
ates at high temperatures must be pro-
tected in the same manner as heater
exhausts; and
(2) Each drain must be protected
from hazardous ice accumulation under
any operating condition.
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as
amended by Amdt. 25–11, 32 FR 6912, May 5,
1967; Amdt. 25–23, 35 FR 5676, Apr. 8, 1970]
§ 25.863
Flammable fluid fire protec-
tion.
(a) In each area where flammable
fluids or vapors might escape by leak-
age of a fluid system, there must be
means to minimize the probability of
ignition of the fluids and vapors, and
the resultant hazards if ignition does
occur.
(b) Compliance with paragraph (a) of
this section must be shown by analysis
or tests, and the following factors must
be considered:
(1) Possible sources and paths of fluid
leakage, and means of detecting leak-
age.
(2) Flammability characteristics of
fluids, including effects of any combus-
tible or absorbing materials.
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