CS 26.155 Flammability
of cargo compartment liners
Compliance with point 26.155 of Part-26 is demonstrated by complying with CS 25.855 & Appendix F Part III, or equivalent or with the following:
(a) Large aeroplanes, Type Certificated after 1 January 1958, with Class C or D compartment, greater than 5.66 m3 (200 cubic feet) have ceiling and sidewall liner panels which are constructed of:
(1) glass fibre reinforced resin, or
(2) materials which meet the flame penetration test specifications of Appendix F Part III, or other equivalent methods, or
(3) aluminium (only in the case of aluminium liner installations approved prior to 1 July 1989).
(b) For compliance with this paragraph, the term ‘liner’ includes any design features, such as a joint or fastener which would affect the capability of the liner to safely contain a fire.
[Issue: 26/3]
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