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131 

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 

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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