CS 22.363 Side load on engine mount

• ED Decision 2003/13/RM found in: Sailplane Rule Book - Part-SAO Part-SFCL CS-22 (Nov 2022)

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.