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Federal Aviation Administration, DOT
§ 125.119
(c) Thermal/acoustic insulation ma-
terials. For transport category air-
planes type certificated after January
1, 1958:
(1) For airplanes manufactured before
September 2, 2005, when thermal/acous-
tic insulation is installed in the fuse-
lage as replacements after September
2, 2005, the insulation must meet the
flame propagation requirements of
§ 25.856 of this chapter, effective Sep-
tember 2, 2003, if it is:
(i) of a blanket construction or
(ii) Installed around air ducting.
(2) For airplanes manufactured after
September 2, 2005, thermal/acoustic in-
sulation materials installed in the fu-
selage must meet the flame propaga-
tion requirements of § 25.856 of this
chapter, effective September 2, 2003.
[Doc. No. 19799, 45 FR 67235, Oct. 9, 1980, as
amended by Amdt. 125–43, 68 FR 45084, July
31, 2003; Amdt. 125–50, 70 FR 77752, Dec. 30,
2005]
§ 125.115
Internal doors.
In any case where internal doors are
equipped with louvres or other ven-
tilating means, there must be a means
convenient to the crew for closing the
flow of air through the door when nec-
essary.
§ 125.117
Ventilation.
Each passenger or crew compartment
must be suitably ventilated. Carbon
monoxide concentration may not be
more than one part in 20,000 parts of
air, and fuel fumes may not be present.
In any case where partitions between
compartments have louvres or other
means allowing air to flow between
compartments, there must be a means
convenient to the crew for closing the
flow of air through the partitions when
necessary.
§ 125.119
Fire precautions.
(a) Each compartment must be de-
signed so that, when used for storing
cargo or baggage, it meets the fol-
lowing requirements:
(1) No compartment may include con-
trols, wiring, lines, equipment, or ac-
cessories that would upon damage or
failure, affect the safe operation of the
airplane unless the item is adequately
shielded, isolated, or otherwise pro-
tected so that it cannot be damaged by
movement of cargo in the compart-
ment and so that damage to or failure
of the item would not create a fire haz-
ard in the compartment.
(2) Cargo or baggage may not inter-
fere with the functioning of the fire-
protective features of the compart-
ment.
(3) Materials used in the construction
of the compartments, including tie-
down equipment, must be at least
flame resistant.
(4) Each compartment must include
provisions for safeguarding against
fires according to the classifications
set forth in paragraphs (b) through (f)
of this section.
(b)
Class A.
Cargo and baggage com-
partments are classified in the ‘‘A’’
category if a fire therein would be
readily discernible to a member of the
crew while at that crewmember’s sta-
tion, and all parts of the compartment
are easily accessible in flight. There
must be a hand fire extinguisher avail-
able for each Class A compartment.
(c)
Class B.
Cargo and baggage com-
partments are classified in the ‘‘B’’
category if enough access is provided
while in flight to enable a member of
the crew to effectively reach all of the
compartment and its contents with a
hand fire extinguisher and the com-
partment is so designed that, when the
access provisions are being used, no
hazardous amount of smoke, flames, or
extinguishing agent enters any com-
partment occupied by the crew or pas-
sengers. Each Class B compartment
must comply with the following:
(1) It must have a separate approved
smoke or fire detector system to give
warning at the pilot or flight engineer
station.
(2) There must be a hand-held fire ex-
tinguisher available for the compart-
ment.
(3) It must be lined with fire-resist-
ant material, except that additional
service lining of flame-resistant mate-
rial may be used.
(d)
Class C.
Cargo and baggage com-
partments are classified in the ‘‘C’’ cat-
egory if they do not conform with the
requirements for the ‘‘A’’, ‘‘B’’, ‘‘D’’, or
‘‘E’’ categories. Each Class C compart-
ment must comply with the following:
(1) It must have a separate approved
smoke or fire detector system to give
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