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CS 25.171 General
Available versions for ERULES-1963177438-8268
ED Decision 2003/2/RM
found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)
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CS 25.171 General ED Decision 2003/2/RM The aeroplane must be longitudinally, directionally and laterally stable in accordance with the provisions of [CS 25.173](#_DxCrossRefBm1709820844) to [25.177](#_DxCrossRefBm1709820694). In addition, suitable stability and control feel (static stability) is required in any condition normally encountered in service, if flight tests show it is necessary for safe operation.