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AMC 22.175 Demonstration of static longitudinal stability
Available versions for ERULES-1963177438-5257
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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AMC 22.175 Demonstration of static longitudinal stability ED Decision 2003/13/RM (1) With air brakes extended, qualitative tests are normally acceptable. (2) Wing-flap positions should include negative positions, where provided. (See [AMC 22.335](#_DxCrossRefBm2056272075))