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139 

Federal Aviation Administration, DOT 

§ 121.340 

must be checked by a designated crew-
member to ensure that each is properly 
stowed and serviceable, and, for other 
than chemical oxygen generator sys-
tems, the breathing gas supply is fully 
charged. Each certificate holder, in its 
operations manual, must designate at 
least one crewmember to perform those 
checks before he or she takes off in 
that airplane for his or her first flight 
of the day. 

[Doc. No. 24792, 52 FR 20957, June 3, 1987, as 
amended by Amdt. 121–204, 54 FR 22271, May 
22, 1989; Amdt. 121–212, 55 FR 5551, Feb. 15, 
1990; Amdt. 121–218, 55 FR 31565, Aug. 2, 1990; 
Amdt. 121–230, 57 FR 42674, Sept. 15, 1992; 
Amdt. 121–251, 60 FR 65932, Dec. 20, 1995; 
Amdt. 121–261, 61 FR 43921, Aug. 26, 1996] 

§ 121.339 Emergency equipment for ex-

tended over-water operations. 

(a) Except where the Administrator, 

by amending the operations specifica-
tions of the certificate holder, requires 
the carriage of all or any specific items 
of the equipment listed below for any 
overwater operation, or upon applica-
tion of the certificate holder, the Ad-
ministrator allows deviation for a par-
ticular extended overwater operation, 
no person may operate an airplane in 
extended overwater operations without 
having on the airplane the following 
equipment: 

(1) A life preserver equipped with an 

approved survivor locator light, for 
each occupant of the airplane. 

(2) Enough life rafts (each equipped 

with an approved survivor locator 
light) of a rated capacity and buoyancy 
to accommodate the occupants of the 
airplane. Unless excess rafts of enough 
capacity are provided, the buoyancy 
and seating capacity beyond the rated 
capacity of the rafts must accommo-
date all occupants of the airplane in 
the event of a loss of one raft of the 
largest rated capacity. 

(3) At least one pyrotechnic signaling 

device for each life raft. 

(4) An approved survival type emer-

gency locator transmitter. Batteries 
used in this transmitter must be re-
placed (or recharged, if the battery is 
rechargeable) when the transmitter has 
been in use for more than 1 cumulative 
hour, or when 50 percent of their useful 
life (or for rechargeable batteries, 50 
percent of their useful life of charge) 

has expired, as established by the 
transmitter manufacturer under its ap-
proval. The new expiration date for re-
placing (or recharging) the battery 
must be legibly marked on the outside 
of the transmitter. The battery useful 
life (or useful life of charge) require-
ments of this paragraph do not apply 
to batteries (such as water-activated 
batteries) that are essentially unaf-
fected during probable storage inter-
vals. 

(b) The required life rafts, life pre-

servers, and survival type emergency 
locator transmitter must be easily ac-
cessible in the event of a ditching with-
out appreciable time for preparatory 
procedures. This equipment must be in-
stalled in conspicuously marked, ap-
proved locations. 

(c) A survival kit, appropriately 

equipped for the route to be flown, 
must be attached to each required life 
raft. 

[Doc. No. 6258, 29 FR 19205, Dec. 31, 1964, as 
amended by Amdt. 121–53, 34 FR 15244, Sept. 
30, 1969; Amdt. 121–79, 36 FR 18724, Sept. 21, 
1971; Amdt. 121–93, 37 FR 14294, June 19, 1972 
Amdt. 121–106, 38 FR 22378, Aug. 20, 1973; 
Amdt. 121–149, 43 FR 50603, Oct. 30, 1978; 
Amdt. 121–158, 45 FR 38348, June 9, 1980; 
Amdt. 121–239, 59 FR 32057, June 21, 1994] 

§ 121.340 Emergency flotation means. 

(a) Except as provided in paragraph 

(b) of this section, no person may oper-
ate an airplane in any overwater oper-
ation unless it is equipped with life 
preservers in accordance with 
§ 121.339(a)(1) or with an approved flota-
tion means for each occupant. This 
means must be within easy reach of 
each seated occupant and must be read-
ily removable from the airplane. 

(b) Upon application by the air car-

rier or commercial operator, the Ad-
ministrator may approve the operation 
of an airplane over water without the 
life preservers or flotation means re-
quired by paragraph (a) of this section, 
if the air carrier or commercial oper-
ator shows that the water over which 
the airplane is to be operated is not of 
such size and depth that life preservers 
or flotation means would be required 
for the survival of its occupants in the 

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140 

14 CFR Ch. I (1–1–24 Edition) 

§ 121.341 

event the flight terminates in that 
water. 

[Doc. No. 6713, 31 FR 1147, Jan. 28, 1966, as 
amended by Amdt. 121–25, 32 FR 3223, Feb. 24, 
1967; Amdt. 121–251, 60 FR 65932, Dec. 20, 1995] 

§ 121.341 Equipment for operations in 

icing conditions. 

(a) Except as permitted in paragraph 

(c)(2) of this section, unless an airplane 
is type certificated under the transport 
category airworthiness requirements 
relating to ice protection, or unless an 
airplane is a non-transport category 
airplane type certificated after Decem-
ber 31, 1964, that has the ice protection 
provisions that meet section 34 of ap-
pendix A of part 135 of this chapter, no 
person may operate an airplane in 
icing conditions unless it is equipped 
with means for the prevention or re-
moval of ice on windshields, wings, em-
pennage, propellers, and other parts of 
the airplane where ice formation will 
adversely affect the safety of the air-
plane. 

(b) No person may operate an air-

plane in icing conditions at night un-
less means are provided for illu-
minating or otherwise determining the 
formation of ice on the parts of the 
wings that are critical from the stand-
point of ice accumulation. Any illu-
minating that is used must be of a type 
that will not cause glare or reflection 
that would handicap crewmembers in 
the performance of their duties. 

(c) 

Non-transport category airplanes 

type certificated after December 31, 1964. 

Except for an airplane that has ice pro-
tection provisions that meet section 34 
of appendix A of part 135 of this chap-
ter, or those for transport category air-
plane type certification, no person may 
operate— 

(1) Under IFR into known or forecast 

light or moderate icing conditions; 

(2) Under VFR into known light or 

moderate icing conditions; unless the 
airplane has functioning deicing anti- 
icing equipment protecting each pro-
peller, windshield, wing, stabilizing or 
control surface, and each airspeed, al-
timeter, rate of climb, or flight atti-
tude instrument system; or 

(3) Into known or forecast severe 

icing conditions. 

(d) If current weather reports and 

briefing information relied upon by the 

pilot in command indicate that the 
forecast icing condition that would 
otherwise prohibit the flight will not 
be encountered during the flight be-
cause of changed weather conditions 
since the forecast, the restrictions in 
paragraph (c) of this section based on 
forecast conditions do not apply. 

[Doc. No. 6258, 29 FR 18205, Dec. 31, 1964, as 
amended by Amdt. 121–251, 60 FR 65929, Dec. 
20, 1995] 

§ 121.342 Pitot heat indication systems. 

No person may operate a transport 

category airplane or, after December 
20, 1999, a nontransport category air-
plane type certificated after December 
31, 1964, that is equipped with a flight 
instrument pitot heating system unless 
the airplane is also equipped with an 
operable pitot heat indication system 
that complies § 25.1326 of this chapter 
in effect on April 12, 1978. 

[Doc. No. 28154, 60 FR 65932, Dec. 20, 1995] 

§ 121.343 Flight data recorders. 

(a) Except as provided in paragraphs 

(b), (c), (d), (e), and (f) of this section, 
no person may operate a large airplane 
that is certificated for operations 
above 25,000 feet altitude or is turbine- 
engine powered unless it is equipped 
with one or more approved flight re-
corders that record data from which 
the following may be determined with-
in the ranges, accuracies, and record-
ing intervals specified in appendix B of 
this part: 

(1) Time; 
(2) Altitude; 
(3) Airspeed; 
(4) Vertical acceleration; 
(5) Heading; and 
(6) Time of each radio transmission 

either to or from air traffic control. 

(b) No person may operate a large 

airplane type certificated up to and in-
cluding September 30, 1969, for oper-
ations above 25,000 feet altitude, or a 
turbine-engine powered airplane cer-
tificated before the same date, unless 
it is equipped before May 26, 1989 with 
one or more approved flight recorders 
that utilize a digital method of record-
ing and storing data and a method of 
readily retrieving that data from the 
storage medium. The following infor-
mation must be able to be determined