Cargo and baggage compartments.

CFR · 2024-01-01 · US · Title 14

For each transport category airplane type certificated after January 1, 1958: (a) Each Class C or Class D compartment, as defined in § 25.857 of this Chapter in effect on June 16, 1986 (see Appendix L to this part), that is greater (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 joint or fastener, which would affect the capability of the liner to safely contain a fire. (c) After March 19, 2001, each Class D compartment, regardless of volume, must meet the standards of §§ 25.857(c) and 25.858 of this Chapter for a Class C compartment unless the operation is an all-cargo operation in which case each Class D compartment may meet the standards in § 25.857(e) for a Class E compartment. (d) (i) The serial number of each airplane listed in the operations specifications issued to the certificate holder for operation under this part in which all Class D compartments have been converted to Class C or Class E compartments; (ii) The serial number of each airplane listed in the operations specification issued to the certificate holder for operation under this part, in which all Class D compartments have been retrofitted to meet the fire detection and suppression requirements for Class C or the fire detection requi

official document · source cfr-2024 · id 14:§ 121.314