Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
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)
Version
CS-25 Amdt 27 - La... (Jan 2023)
Section
Share
Version
Show details
Hide details
Version
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.