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CS 22.421 Balancing loads
Available versions for ERULES-1963177438-5351
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 22.421 Balancing loads ED Decision 2003/13/RM (a) A horizontal tail balancing load is the load necessary to maintain equilibrium in any specified flight condition with no pitching acceleration. (b) The horizontal tail must be designed for the balancing loads occurring at any point of the limit manoeuvring envelope and in the air-brake and wing-flap positions as specified in [CS 22.333](#_DxCrossRefBm2056272107) and [CS 22.345](#_DxCrossRefBm2056272106).