Section 121.314 14 CFR Ch. I (1-1-19 Edition) pilot-s permission, except that nontransport category airplanes certificated after December 31, 1964, are not required to comply with this paragraph. For airplanes equipped with a crew rest area having separate entries from the flightdeck and the passenger compartment, a door with such a locking means must be provided between the crew rest area and the passenger compartment. (g) A key for each door that separates a passenger compartment from another compartment that has emergency 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 perform 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 internal flightdeck locking device installed, 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 landing. (i) A means for the crew, in an emergency to unlock each door that leads to a compartment that is normally accessible to passengers and that can be locked by passengers. (j) After April 9, 2003, for airplanes required by paragraph (f) of this section to have a door between the passenger and pilot or crew rest compartments, and for transport category, allcargo airplanes that have a door installed 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 section to have a door between the passenger and pilot or crew rest compartments, (i) Each such door must meet the requirements of Section 25.795(a)(1) and (2) in effect 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 becomes 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 compartment and any other occupied compartment on or after January 15, 2002, each such door must meet the requirements of Section 25.795(a)(1) and (2) in effect on January 15, 2002; or the operator must implement a security program approved by the Transportation Security Administration (TSA) for the operation of all airplanes in that operator-s fleet. (k) Except for all-cargo operations as defined in Section 110.2 of this chapter, for all passenger-carrying airplanes that require a lockable flightdeck door in accordance with paragraph (f) of this section, 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] Section 121.314 Cargo and baggage compartments. For each transport category airplane type certificated after January 1, 1958: (a) Each Class C or Class D compartment, as defined in Section 25.857 of this Chapter in effect on June 16, 1986 (see Appendix 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 requirements of part 25, appendix F, part III of this chapter; or (3) In the case of liner installations approved prior to March 20, 1989, aluminum. (b) For compliance with paragraph (a) of this section, the term - liner - includes any design feature, such as a 116 VerDate Sep<11>2014 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00126 Fmt 8010 Sfmt 8010 Y:\SGML\247048.XXX 247048