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14 CFR Ch. I (1–1–24 Edition)
§ 29.1194
supported so that it can resist the vi-
bration, inertia, and air loads to which
it may be subjected in operation.
(b) Cowling must meet the drainage
and ventilation requirements of
§ 29.1187.
(c) On rotorcraft with a diaphragm
isolating the engine power section from
the engine accessory section, each part
of the accessory section cowling sub-
ject to flame in case of fire in the en-
gine power section of the powerplant
must—
(1) Be fireproof; and
(2) Meet the requirements of § 29.1191.
(d) Each part of the cowling or engine
compartment covering subject to high
temperatures due to its nearness to ex-
haust system parts or exhaust gas im-
pingement must be fireproof.
(e) Each rotorcraft must—
(1) Be designated and constructed so
that no fire originating in any fire zone
can enter, either through openings or
by burning through external skin, any
other zone or region where it would
create additional hazards;
(2) Meet the requirements of para-
graph (e)(1) of this section with the
landing gear retracted (if applicable);
and
(3) Have fireproof skin in areas sub-
ject to flame if a fire starts in or burns
out of any designated fire zone.
(f) A means of retention for each
openable or readily removable panel,
cowling, or engine or rotor drive sys-
tem covering must be provided to pre-
clude hazardous damage to rotors or
critical control components in the
event of—
(1) Structural or mechanical failure
of the normal retention means, unless
such failure is extremely improbable;
or
(2) Fire in a fire zone, if such fire
could adversely affect the normal
means of retention.
(Secs. 313(a), 601, and 603, 72 Stat. 759, 775, 49
U.S.C. 1354(a), 1421, and 1423; sec. 6(c), 49
U.S.C. 1655(c))
[Doc. No. 5084, 29 FR 16150, Dec. 3, 1964, as
amended by Amdt. 29–3, 33 FR 970, Jan. 26,
1968; Amdt. 29–13, 42 FR 15046, Mar. 17, 1977;
Amdt. 29–26, 53 FR 34219, Sept. 2, 1988]
§ 29.1194
Other surfaces.
All surfaces aft of, and near, engine
compartments and designated fire
zones, other than tail surfaces not sub-
ject to heat, flames, or sparks ema-
nating from a designated fire zone or
engine compartment, must be at least
fire resistant.
[Amdt. 29–3, 33 FR 970, Jan. 26, 1968]
§ 29.1195
Fire extinguishing systems.
(a) Each turbine engine powered
rotorcraft and Category A recipro-
cating engine powered rotorcraft, and
each Category B reciprocating engine
powered rotorcraft with engines of
more than 1,500 cubic inches must have
a fire extinguishing system for the des-
ignated fire zones. The fire extin-
guishing system for a powerplant must
be able to simultaneously protect all
zones of the powerplant compartment
for which protection is provided.
(b) For multiengine powered rotor-
craft, the fire extinguishing system,
the quantity of extinguishing agent,
and the rate of discharge must—
(1) For each auxiliary power unit and
combustion equipment, provide at least
one adequate discharge; and
(2) For each other designated fire
zone, provide two adequate discharges.
(c) For single engine rotorcraft, the
quantity of extinguishing agent and
the rate of discharge must provide at
least one adequate discharge for the
engine compartment.
(d) It must be shown by either actual
or simulated flight tests that under
critical airflow conditions in flight the
discharge of the extinguishing agent in
each designated fire zone will provide
an agent concentration capable of ex-
tinguishing fires in that zone and of
minimizing the probability of reigni-
tion.
(Secs. 313(a), 601, 603, 604, Federal Aviation
Act of 1958 (49 U.S.C. 1354(a), 1421, 1423, 1424),
sec. 6(c), Dept. of Transportation Act (49
U.S.C. 1655(c)))
[Doc. No. 5084, 29 FR 16150, Dec. 3, 1964, as
amended by Amdt. 29–3, 33 FR 970, Jan. 26,
1968; Amdt. 29–13, 42 FR 15047, Mar. 17, 1977;
Amdt. 29–17, 43 FR 50602, Oct. 30, 1978]
§ 29.1197
Fire extinguishing agents.
(a) Fire extinguishing agents must—
(1) Be capable of extinguishing
flames emanating from any burning of
fluids or other combustible materials
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