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Federal Aviation Administration, DOT
§ 121.321
handsets, headsets, microphones, selec-
tor switches, and signaling devices;
(b) Is approved in accordance with
§ 21.305 of this chapter;
(c) Is accessible for immediate use
from each of two flight crewmember
stations in the pilot compartment;
(d) For each required floor-level pas-
senger emergency exit which has an ad-
jacent flight attendant seat, has a
microphone which is readily accessible
to the seated flight attendant, except
that one microphone may serve more
than one exit, provided the proximity
of the exits allows unassisted verbal
communication between seated flight
attendants;
(e) Is capable of operation within 10
seconds by a flight attendant at each of
those stations in the passenger com-
partment from which its use is acces-
sible;
(f) Is audible at all passenger seats,
lavatories, and flight attendant seats
and work stations; and
(g) For transport category airplanes
manufactured on or after November 27,
1990, meets the requirements of § 25.1423
of this chapter.
[Doc. No. 24995, 54 FR 43926, Oct. 27, 1989]
§ 121.319 Crewmember interphone sys-
tem.
(a) No person may operate an air-
plane with a seating capacity of more
than 19 passengers unless the airplane
is equipped with a crewmember inter-
phone system that:
(1) [Reserved]
(2) Is capable of operation inde-
pendent of the public address system
required by § 121.318(a) except for
handsets, headsets, microphones, selec-
tor switches, and signaling devices; and
(3) Meets the requirements of para-
graph (b) of this section.
(b) The crewmember interphone sys-
tem required by paragraph (a) of this
section must be approved in accordance
with § 21.305 of this chapter and meet
the following requirements:
(1) It must provide a means of two-
way communication between the pilot
compartment and—
(i) Each passenger compartment; and
(ii) Each galley located on other than
the main passenger deck level.
(2) It must be accessible for imme-
diate use from each of two flight crew-
member stations in the pilot compart-
ment;
(3) It must be accessible for use from
at least one normal flight attendant
station in each passenger compart-
ment;
(4) It must be capable of operation
within 10 seconds by a flight attendant
at those stations in each passenger
compartment from which its use is ac-
cessible; and
(5) For large turbojet-powered air-
planes:
(i) It must be accessible for use at
enough flight attendant stations so
that all floor-level emergency exits (or
entryways to those exits in the case of
exits located within galleys) in each
passenger compartment are observable
from one or more of those stations so
equipped;
(ii) It must have an alerting system
incorporating aural or visual signals
for use by flight crewmembers to alert
flight attendants and for use by flight
attendants to alert flight crew-
members;
(iii) The alerting system required by
paragraph (b)(5)(ii) of this section must
have a means for the recipient of a call
to determine whether it is a normal
call or an emergency call; and
(iv) When the airplane is on the
ground, it must provide a means of
two-way communication between
ground personnel and either of at least
two flight crewmembers in the pilot
compartment. The interphone system
station for use by ground personnel
must be so located that personnel
using the system may avoid visible de-
tection from within the airplane.
[Doc. No. 10865, 38 FR 21494, Aug. 9, 1973, as
amended by Amdt. 121–121, 40 FR 42186, Sept.
11, 1975; Amdt. 121–149, 43 FR 50602, Oct. 30,
1978; Amdt. 121–178, 47 FR 13316, Mar. 29, 1982;
Amdt. 121–253, 61 FR 2611, Jan. 26, 1996]
§ 121.321 Operations in icing.
After October 21, 2013, no person may
operate an airplane with a certificated
maximum takeoff weight less than
60,000 pounds in conditions conducive
to airframe icing unless it complies
with this section. As used in this sec-
tion, the phrase ‘‘conditions conducive
to airframe icing’’ means visible mois-
ture at or below a static air tempera-
ture of 5
°
C or a total air temperature
132
14 CFR Ch. I (1–1–24 Edition)
§ 121.323
of 10
°
C, unless the approved Airplane
Flight Manual provides another defini-
tion.
(a) When operating in conditions con-
ducive to airframe icing, compliance
must be shown with paragraph (a)(1),
or (2), or (3) of this section.
(1) The airplane must be equipped
with a certificated primary airframe
ice detection system.
(i) The airframe ice protection sys-
tem must be activated automatically,
or manually by the flightcrew, when
the primary ice detection system indi-
cates activation is necessary.
(ii) When the airframe ice protection
system is activated, any other proce-
dures in the Airplane Flight Manual
for operating in icing conditions must
be initiated.
(2) Visual cues of the first sign of ice
formation anywhere on the airplane
and a certificated advisory airframe ice
detection system must be provided.
(i) The airframe ice protection sys-
tem must be activated when any of the
visual cues are observed or when the
advisory airframe ice detection system
indicates activation is necessary,
whichever occurs first.
(ii) When the airframe ice protection
system is activated, any other proce-
dures in the Airplane Flight Manual
for operating in icing conditions must
be initiated.
(3) If the airplane is not equipped to
comply with the provisions of para-
graph (a)(1) or (2) of this section, then
the following apply:
(i) When operating in conditions con-
ducive to airframe icing, the airframe
ice protection system must be acti-
vated prior to, and operated during, the
following phases of flight:
(A) Takeoff climb after second seg-
ment,
(B) En route climb,
(C) Go-around climb,
(D) Holding,
(E) Maneuvering for approach and
landing, and
(F) Any other operation at approach
or holding airspeeds.
(ii) During any other phase of flight,
the airframe ice protection system
must be activated and operated at the
first sign of ice formation anywhere on
the airplane, unless the Airplane
Flight Manual specifies that the air-
frame ice protection system should not
be used or provides other operational
instructions.
(iii) Any additional procedures for
operation in conditions conducive to
icing specified in the Airplane Flight
Manual or in the manual required by
§ 121.133 must be initiated.
(b) If the procedures specified in
paragraph (a)(3)(i) of this section are
specifically prohibited in the Airplane
Flight Manual, compliance must be
shown with the requirements of para-
graph (a)(1) or (2) of this section.
(c) Procedures necessary for safe op-
eration of the airframe ice protection
system must be established and docu-
mented in:
(1) The Airplane Flight Manual for
airplanes that comply with paragraph
(a)(1) or (2) of this section, or
(2) The Airplane Flight Manual or in
the manual required by § 121.133 for air-
planes that comply with paragraph
(a)(3) of this section.
(d) Procedures for operation of the
airframe ice protection system must
include initial activation, operation
after initial activation, and deactiva-
tion. Procedures for operation after
initial activation of the ice protection
system must address—
(1) Continuous operation,
(2) Automatic cycling,
(3) Manual cycling if the airplane is
equipped with an ice detection system
that alerts the flightcrew each time
the ice protection system must be cy-
cled, or
(4) Manual cycling based on a time
interval if the airplane type is not
equipped with features necessary to
implement (d)(1)–(3) of this section.
(e) System installations used to com-
ply with paragraph (a)(1) or (a)(2) of
this section must be approved through
an amended or supplemental type cer-
tificate in accordance with part 21 of
this chapter.
[Doc. No. FAA–2009–0675, 78 FR 15876, Mar. 13,
2013]
§ 121.323 Instruments and equipment
for operations at night.
No person may operate an airplane at
night under this part unless it is
equipped with the following instru-
ments and equipment in addition to