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Federal Aviation Administration, DOT
§ 121.309
turbine engine powered airplanes to
provide equivalent safety, no person
may conduct any operation under this
part without the following engine in-
struments:
(a) A carburetor air temperature in-
dicator for each engine.
(b) A cylinder head temperature indi-
cator for each air-cooled engine.
(c) A fuel pressure indicator for each
engine.
(d) A fuel flowmeter or fuel mixture
indicator for each engine not equipped
with an automatic altitude mixture
control.
(e) A means for indicating fuel quan-
tity in each fuel tank to be used.
(f) A manifold pressure indicator for
each engine.
(g) An oil pressure indicator for each
engine.
(h) An oil quantity indicator for each
oil tank when a transfer or separate oil
reserve supply is used.
(i) An oil-in temperature indicator
for each engine.
(j) A tachometer for each engine.
(k) An independent fuel pressure
warning device for each engine or a
master warning device for all engines
with a means for isolating the indi-
vidual warning circuits from the mas-
ter warning device.
(l) A device for each reversible pro-
peller, to indicate to the pilot when the
propeller is in reverse pitch, that com-
plies with the following:
(1) The device may be actuated at
any point in the reversing cycle be-
tween the normal low pitch stop posi-
tion and full reverse pitch, but it may
not give an indication at or above the
normal low pitch stop position.
(2) The source of indication must be
actuated by the propeller blade angle
or be directly responsive to it.
§ 121.308 Lavatory fire protection.
(a) Except as provided in paragraphs
(c) and (d) of this section, no person
may operate a passenger-carrying air-
plane unless each lavatory in the air-
plane is equipped with a smoke detec-
tor system or equivalent that provides
a warning light in the cockpit or pro-
vides a warning light or audio warning
in the passenger cabin which would be
readily detected by a flight attendant,
taking into consideration the posi-
tioning of flight attendants throughout
the passenger compartment during var-
ious phases of flight.
(b) Except as provided in paragraph
(c) of this section, no person may oper-
ate a passenger-carrying airplane un-
less each lavatory in the airplane is
equipped with a built-in fire extin-
guisher for each disposal receptacle for
towels, paper, or waste located within
the lavatory. The built-in fire extin-
guisher must be designed to discharge
automatically into each disposal recep-
tacle upon occurrence of a fire in the
receptacle.
(c) Until December 22, 1997, a certifi-
cate holder described in § 121.2(a) (1) or
(2) may operate an airplane with a pas-
senger seat configuration of 30 or fewer
seats that does not comply with the
smoke detector system requirements
described in paragraph (a) of this sec-
tion and the fire extinguisher require-
ments described in paragraph (b) of
this section.
(d) After December 22, 1997, no person
may operate a nontransport category
airplane type certificated after Decem-
ber 31, 1964, with a passenger seat con-
figuration of 10–19 seats unless that
airplane complies with the smoke de-
tector system requirements described
in paragraph (a) of this section, except
that the smoke detector system or
equivalent must provide a warning
light in the cockpit or an audio warn-
ing that would be readily detected by
the flightcrew.
[Doc. No. 28154, 60 FR 65929, Dec. 20, 1995]
§ 121.309 Emergency equipment.
(a)
General:
No person may operate
an airplane unless it is equipped with
the emergency equipment listed in this
section and in § 121.310.
(b) Each item of emergency and flo-
tation equipment listed in this section
and in §§ 121.310, 121.339, and 121.340—
(1) Must be inspected regularly in ac-
cordance with inspection periods estab-
lished in the operations specifications
to ensure its condition for continued
serviceability and immediate readiness
to perform its intended emergency pur-
poses;
(2) Must be readily accessible to the
crew and, with regard to equipment lo-
cated in the passenger compartment,
to passengers;