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CS 25.363 Side load on engine and auxiliary power unit mounts
Available versions for ERULES-1963177438-8387
ED Decision 2003/2/RM
found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)
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CS-25 Amdt 27 - La... (Jan 2023)
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CS 25.363 Side load on engine and auxiliary power unit mounts ED Decision 2003/2/RM (a) Each engine and auxiliary power unit mount and its supporting structure must be designed for a limit load factor in a lateral direction, for the side load on the engine and auxiliary power unit mount, at least equal to the maximum load factor obtained in the yawing conditions but not less than – (1) 1·33; or (2) One-third of the limit load factor for flight condition A as prescribed in [CS 25.333(b)](#_DxCrossRefBm1709820896). (b) The side load prescribed in sub-paragraph (a) of this paragraph may be assumed to be independent of other flight conditions.