CS 26.155 Flammability of cargo compartment liners

• ED Decision 2020/023/R found in: CS-26 Additional Airworthiness Specifications for Operations (No 2015/640) Part-26 (Mar 2023)

CS 26.155 Flammability of cargo compartment liners ED Decision 2020/023/R Compliance with point [26.155](#_DxCrossRefBm881534029) of Part-26 is demonstrated by complying with CS 25.855 & [Appendix F Part III](#_DxCrossRefBm881534143), 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](#_DxCrossRefBm881534143), 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]