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Federal Aviation Administration, DOT
§ 125.189
means for proper notification of the
passenger is provided.
(c) All cargo may be carried forward
of the foremost seated passengers and
carry-on baggage may be carried along-
side the foremost seated passengers if
the cargo (including carry-on baggage)
is carried either in approved bins as
specified in paragraph (b) of this sec-
tion or in accordance with the fol-
lowing:
(1) It is properly secured by a safety
belt or other tie down having enough
strength to eliminate the possibility of
shifting under all normally anticipated
flight and ground conditions.
(2) It is packaged or covered in a
manner to avoid possible injury to pas-
sengers.
(3) It does not impose any load on
seats or the floor structure that ex-
ceeds the load limitation for those
components.
(4) Its location does not restrict ac-
cess to or use of any required emer-
gency or regular exit, or of the aisle in
the passenger compartment.
(5) Its location does not obscure any
passenger’s view of the ‘‘seat belt’’
sign, ‘‘no smoking’’ sign, or required
exit sign, unless an auxiliary sign or
other approved means for proper notifi-
cation of the passenger is provided.
§ 125.185 Carriage of cargo in cargo
compartments.
When cargo is carried in cargo com-
partments that are designed to require
the physical entry of a crewmember to
extinguish any fire that may occur
during flight, the cargo must be loaded
so as to allow a crewmember to effec-
tively reach all parts of the compart-
ment with the contents of a hand-held
fire extinguisher.
§ 125.187 Landing gear: Aural warning
device.
(a) Except for airplanes that comply
with the requirements of § 25.729 of this
chapter on or after January 6, 1992,
each airplane must have a landing gear
aural warning device that functions
continuously under the following con-
ditions:
(1) For airplanes with an established
approach wing-flap position, whenever
the wing flaps are extended beyond the
maximum certificated approach climb
configuration position in the Airplane
Flight Manual and the landing gear is
not fully extended and locked.
(2) For airplanes without an estab-
lished approach climb wing-flap posi-
tion, whenever the wing flaps are ex-
tended beyond the position at which
landing gear extension is normally per-
formed and the landing gear is not
fully extended and locked.
(b) The warning system required by
paragraph (a) of this section—
(1) May not have a manual shutoff;
(2) Must be in addition to the throt-
tle-actuated device installed under the
type certification airworthiness re-
quirements; and
(3) May utilize any part of the throt-
tle-actuated system including the
aural warning device.
(c) The flap position sensing unit
may be installed at any suitable place
in the airplane.
[Doc. No. 19779, 45 FR 67235, Oct. 9, 1980, as
amended by Amdt. 125–16, 56 FR 63762, Dec. 5,
1991]
§ 125.189 Demonstration of emergency
evacuation procedures.
(a) Each certificate holder must
show, by actual demonstration con-
ducted in accordance with paragraph
(a) of appendix B of this part, that the
emergency evacuation procedures for
each type and model of airplane with a
seating of more than 44 passengers,
that is used in its passenger-carrying
operations, allow the evacuation of the
full seating capacity, including crew-
members, in 90 seconds or less, in each
of the following circumstances:
(1) A demonstration must be con-
ducted by the certificate holder upon
the initial introduction of a type and
model of airplane into passenger-car-
rying operations. However, the dem-
onstration need not be repeated for any
airplane type or model that has the
same number and type of exits, the
same cabin configuration, and the
same emergency equipment as any
other airplane used by the certificate
holder in successfully demonstrating
emergency evacuation in compliance
with this paragraph.
(2) A demonstration must be con-
ducted—
(i) Upon increasing by more than 5
percent the passenger seating capacity