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CS 25.457 Wing-flaps
Available versions for ERULES-1963177438-8451
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 25.457 Wing-flaps ED Decision 2003/2/RM Wing flaps, their operating mechanisms, and their supporting structures must be designed for critical loads occurring in the conditions prescribed in [CS 25.345](#_DxCrossRefBm1709820949), accounting for the loads occurring during transition from one wing-flap position and airspeed to another.