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CS 22.423 Manoeuvring loads
Available versions for ERULES-1963177438-5352
ED Decision 2003/13/RM
found in: Sailplane Rule Book - Part-SAO Part-SFCL CS-22 (Nov 2022)
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Sailplane Rule Boo... (Nov 2022)
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CS 22.423 Manoeuvring loads ED Decision 2003/13/RM The horizontal tail must be designed for the most severe loads likely to occur in pilot-induced pitching manoeuvres, at all speeds up to VD.