151
Federal Aviation Administration, DOT
§ 121.354
(3) At least one of the communica-
tion systems must have two-way voice
communication capability.
(b) No certificate holder conducting a
flag or supplemental operation or a do-
mestic operation within the State of
Alaska may conduct an operation with-
out the equipment specified in para-
graph (a) of this section, if the Admin-
istrator finds that equipment to be
necessary for search and rescue oper-
ations because of the nature of the ter-
rain to be flown over.
(c) Notwithstanding the require-
ments of paragraph (a) of this section,
installation and use of a single LRNS
and a single LRCS may be authorized
by the Administrator and approved in
the certificate holder’s operations
specifications for operations and routes
in certain geographic areas. The fol-
lowing are among the operational fac-
tors the Administrator may consider in
granting an authorization:
(1) The ability of the flightcrew to
navigate the airplane along the route
within the degree of accuracy required
for ATC,
(2) The length of the route being
flown, and
(3) The duration of the very high fre-
quency communications gap.
[Doc. No. 6258, 29 FR 19205, Dec. 31, 1964, as
amended by Amdt. 121–253, 61 FR 2611, Jan.
26, 1996; Amdt. 121–254, 61 FR 7191, Feb. 26,
1996; Amdt. 121–333, 72 FR 31682, June 7, 2007]
§ 121.353 Emergency equipment for op-
erations over uninhabited terrain
areas: Flag, supplemental, and cer-
tain domestic operations.
Unless the airplane has the following
equipment, no person may conduct a
flag or supplemental operation or a do-
mestic operation within the States of
Alaska or Hawaii over an uninhabited
area or any other area that (in its oper-
ations specifications) the Adminis-
trator specifies required equipment for
search and rescue in case of an emer-
gency:
(a) Suitable pyrotechnic signaling de-
vices.
(b) 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.
(c) Enough survival kits, appro-
priately equipped for the route to be
flown for the number of occupants of
the airplane.
[Doc. No. 6258, 29 FR 19205, Dec. 31, 1964, as
amended by Amdt. 121–79, 36 FR 18724, Sept.
21, 1971; Amdt. 121–106, 38 FR 22378 Aug. 20,
1973; Amdt. 121–158, 45 FR 38348, June 9, 1980;
Amdt. 121–239, 59 FR 32057, June 21, 1994;
Amdt. 121–251, 60 FR 65932, Dec. 20, 1995]
§ 121.354 Terrain awareness and warn-
ing system.
(a)
Airplanes manufactured after March
29, 2002.
No person may operate a tur-
bine-powered airplane unless that air-
plane is equipped with an approved ter-
rain awareness and warning system
that meets the requirements for Class
A equipment in Technical Standard
Order (TSO)–C151. The airplane must
also include an approved terrain situa-
tional awareness display.
(b)
Airplanes manufactured on or before
March 29, 2002.
No person may operate
a turbine-powered airplane after March
29, 2005, unless that airplane is
equipped with an approved terrain
awareness and warning system that
meets the requirements for Class A
equipment in Technical Standard Order
(TSO)–C151. The airplane must also in-
clude an approved terrain situational
awareness display.
(Approved by the Office of Management and
Budget under control number 2120–0631)
(c)
Airplane Flight Manual.
The Air-
plane Flight Manual shall contain ap-
propriate procedures for—
(1) The use of the terrain awareness
and warning system; and
(2) Proper flight crew reaction in re-
sponse to the terrain awareness and
152
14 CFR Ch. I (1–1–24 Edition)
§ 121.355
warning system audio and visual warn-
ings.
[Doc. No. 29312, 65 FR 16755, Mar. 29, 2000]
§ 121.355 Equipment for operations on
which specialized means of naviga-
tion are used.
(a) No certificate holder may conduct
an operation—
(1) Using Doppler Radar or an Iner-
tial Navigation System outside the 48
contiguous States and the District of
Columbia, unless such systems have
been approved in accordance with ap-
pendix G to this part; or
(2) Using Doppler Radar or an Iner-
tial Navigation System within the 48
contiguous States and the District of
Columbia, or any other specialized
means of navigation, unless it shows
that an adequate airborne system is
provided for the specialized navigation
authorized for the particular operation.
(b) Notwithstanding paragraph (a) of
this section, Doppler Radar and Iner-
tial Navigation Systems, and the train-
ing programs, maintenance programs,
relevant operations manual material,
and minimum equipment lists prepared
in accordance therewith, approved be-
fore April 29, 1972, are not required to
be approved in accordance with that
paragraph.
[Doc. No. 10204, 37 FR 6464, Mar. 30, 1972]
§ 121.356 Collision avoidance system.
Effective January 1, 2005, any air-
plane you operate under this part must
be equipped and operated according to
the following table:
C
OLLISION
A
VOIDANCE
S
YSTEMS
If you operate any—
Then you must operate that airplane
with—
(a) Turbine-powered
airplane of more
than 33,000
pounds maximum
certificated take-
off weight.
(1) An appropriate class of Mode S
transponder that meets Technical
Standard Order (TSO) C–112, or a
later version, and one of the fol-
lowing approved units:
(i) TCAS II that meets TSO C–119b
(version 7.0), or takeoff weight a
later version.
C
OLLISION
A
VOIDANCE
S
YSTEMS
—Continued
If you operate any—
Then you must operate that airplane
with—
(ii) TCAS II that meets TSO C–119a
(version 6.04A Enhanced) that was
installed in that airplane before May
1, 2003. If that TCAS II version
6.04A Enhanced no longer can be
repaired to TSO C–119a standards,
it must be replaced with a TCAS II
that meets TSO C–119b (version
7.0), or a later version.
(iii) A collision avoidance system equiv-
alent to TSO C–119b (version 7.0),
or a later version, capable of coordi-
nating with units that meet TSO C–
119a (version 6.04A Enhanced), or a
later version.
(b) Passenger or
combination
cargo/passenger
(combi) airplane
that has a pas-
senger seat con-
figuration of 10–
30 seats.
(1) TCAS I that meets TSO C–118, or
a later version, or
(2) A collision avoidance system equiv-
alent to has a TSO C–118, or a later
version, or
(3) A collision avoidance system and
Mode S transponder that meet para-
graph (a)(1) of this section.
(c) Piston-powered
airplane of more
than 33,000
pounds maximum
certificated take-
off weight.
(1) TCAS I that meets TSO C–118, or
a later version, or
(2) A collision avoidance system equiv-
alent to maximum TSO C–118, or a
later version, or
(3) A collision avoidance system and
Mode S transponder that meet para-
graph (a)(1) of this section.
[Doc. No. FAA–2001–10910, 68 FR 15902, Apr. 1,
2003]
§ 121.357 Airborne weather radar
equipment requirements.
(a) No person may operate any trans-
port category airplane (except C–46
type airplanes) or a nontransport cat-
egory airplane certificated after De-
cember 31, 1964, unless approved air-
borne weather radar equipment has
been installed in the airplane.
(b) [Reserved]
(c) Each person operating an airplane
required to have approved airborne
weather radar equipment installed
shall, when using it under this part, op-
erate it in accordance with the fol-
lowing:
(1)
Dispatch.
No person may dispatch
an airplane (or begin the flight of an
airplane in the case of a certificate
holder, that does not use a dispatch
system) under IFR or night VFR condi-
tions when current weather reports in-
dicate that thunderstorms, or other po-
tentially hazardous weather conditions
that can be detected with airborne