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CS 25.391 Control surface loads: general
Available versions for ERULES-1963177438-9393
ED Decision 2005/006/R
found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)
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CS-25 Amdt 27 - La... (Jan 2023)
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CS 25.391 Control surface loads: general ED Decision 2005/006/R The control surfaces must be designed for the limit loads resulting from the flight conditions in [CS 25.331](#_DxCrossRefBm1709820915), [CS 25.341(a) and (b)](#_DxCrossRefBm1709820927), [CS 25.349](#_DxCrossRefBm1709820948) and [CS 25.351](#_DxCrossRefBm1709820961), considering the requirements for: (a) Loads parallel to hinge line, in [CS 25.393](#_DxCrossRefBm1709820985); (b) Pilot effort effects, in [CS 25.397](#_DxCrossRefBm1709820894); (c) Trim tab effects, in [CS 25.407](#_DxCrossRefBm1709820984); (d) Unsymmetrical loads, in [CS 25.427](#_DxCrossRefBm1709820945); and (e) Auxiliary aerodynamic surfaces, in [CS 25.445](#_DxCrossRefBm1709820944). [Amdt 25/1]