116
14 CFR Ch. I (1–1–19 Edition)
§ 121.314
pilot’s permission, except that non-
transport category airplanes certifi-
cated after December 31, 1964, are not
required to comply with this para-
graph. For airplanes equipped with a
crew rest area having separate entries
from the flightdeck and the passenger
compartment, a door with such a lock-
ing means must be provided between
the crew rest area and the passenger
compartment.
(g) A key for each door that sepa-
rates a passenger compartment from
another compartment that has emer-
gency exit provisions. Except for
flightdeck doors, a key must be readily
available for each crewmember. Except
as provided below, no person other
than a person who is assigned to per-
form duty on the flightdeck may have
a key to the flightdeck door. Before
April 22, 2003, any crewmember may
have a key to the flightdeck door but
only if the flightdeck door has an in-
ternal flightdeck locking device in-
stalled, operative, and in use. Such
‘‘internal flightdeck locking device’’
has to be designed so that it can only
be unlocked from inside the flightdeck.
(h) A placard on each door that is the
means of access to a required passenger
emergency exit, to indicate that it
must be open during takeoff and land-
ing.
(i) A means for the crew, in an emer-
gency to unlock each door that leads to
a compartment that is normally acces-
sible to passengers and that can be
locked by passengers.
(j) After April 9, 2003, for airplanes
required by paragraph (f) of this sec-
tion to have a door between the pas-
senger and pilot or crew rest compart-
ments, and for transport category, all-
cargo airplanes that have a door in-
stalled between the pilot compartment
and any other occupied compartment
on January 15, 2002;
(1) After April 9, 2003, for airplanes
required by paragraph (f) of this sec-
tion to have a door between the pas-
senger and pilot or crew rest compart-
ments,
(i) Each such door must meet the re-
quirements of § 25.795(a)(1) and (2) in ef-
fect on January 15, 2002; and
(ii) Each operator must establish
methods to enable a flight attendant to
enter the pilot compartment in the
event that a flightcrew member be-
comes incapacitated. Any associated
signal or confirmation system must be
operable by each flightcrew member
from that flightcrew member’s duty
station.
(2) After October 1, 2003, for transport
category, all-cargo airplanes that had a
door installed between the pilot com-
partment and any other occupied com-
partment on or after January 15, 2002,
each such door must meet the require-
ments of § 25.795(a)(1) and (2) in effect
on January 15, 2002; or the operator
must implement a security program
approved by the Transportation Secu-
rity Administration (TSA) for the oper-
ation of all airplanes in that operator’s
fleet.
(k) Except for all-cargo operations as
defined in § 110.2 of this chapter, for all
passenger-carrying airplanes that re-
quire a lockable flightdeck door in ac-
cordance with paragraph (f) of this sec-
tion, a means to monitor from the
flightdeck side of the door the area
outside the flightdeck door to identify
persons requesting entry and to detect
suspicious behavior and potential
threats.
[Doc. No. 6258, 29 FR 19205, Dec. 31, 1964, as
amended by Amdt. 121–5, 30 FR 6113, Apr. 30,
1965; Amdt. 121–251, 60 FR 65931, Dec. 20, 1995;
Amdt. 121–288, 67 FR 2127, Jan. 15, 2002; Amdt.
121–299, 68 FR 42881, July 18, 2003; Amdt. 121–
334, 72 FR 45635, Aug. 15, 2007; Amdt. 121–353,
76 FR 7488, Feb. 10, 2011]
§ 121.314
Cargo and baggage compart-
ments.
For each transport category airplane
type certificated after January 1, 1958:
(a) Each Class C or Class D compart-
ment, as defined in § 25.857 of this Chap-
ter in effect on June 16, 1986 (see Ap-
pendix L to this part), that is greater
than 200 cubic feet in volume must
have ceiling and sidewall liner panels
which are constructed of:
(1) Glass fiber reinforced resin;
(2) Materials which meet the test re-
quirements of part 25, appendix F, part
III of this chapter; or
(3) In the case of liner installations
approved prior to March 20, 1989, alu-
minum.
(b) For compliance with paragraph
(a) of this section, the term ‘‘liner’’ in-
cludes any design feature, such as a
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