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CS 22.447 Combined loads on tail surfaces
Available versions for ERULES-1963177438-5358
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 22.447 Combined loads on tail surfaces ED Decision 2003/13/RM (a) The unsymmetrical distribution of the balancing load on the horizontal tail which arises in flight conditions A and D of the V-n envelope must be combined with the appropriate manoeuvring load on the vertical surface as specified in [CS 22.441](#_DxCrossRefBm2056272122) acting in such a direction as to increase the rolling torque. (b) 75% for Category U and 100% for Category A of the loads according to [CS 22.423](#_DxCrossRefBm2056272144) for the horizontal tail and [CS 22.441](#_DxCrossRefBm2056272122) for the vertical tail must be assumed to be acting simultaneously.