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CS 22.371 Gyroscopic Loads
Available versions for ERULES-1963177438-5342
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 22.371 Gyroscopic Loads ED Decision 2003/13/RM For powered sailplanes of airworthiness Category A, the engine mount and its supporting structure must be designed for gyroscopic loads resulting from maximum continuous r.p.m.