CS
22.363 Side load on engine mount
ED Decision 2003/13/RM
(a) The engine mount and its supporting structure must be designed for a limit load factor in a lateral direction, for the side load on the engine mount, of not less than one-third of the limit load factor for flight condition A (1/3 n1).
(b) The side load prescribed in (a) may be assumed to be independent of other flight conditions.
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