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CS 25.181 Dynamic stability

Large Aeroplanes (CS-25) · CS-25 · EAR revision 26 Jan 2023

IRImplementing rule

CS 25.181Dynamic stability

(See AMC 25.181)

(a)Any short period oscillation, not including combined lateral-directional oscillations, occurring between 1·13 VSR and maximum allowable speed appropriate to the configuration of the aeroplane must be heavily damped with the primary controls –

(1)Free; and

(2)In a fixed position.

(b)Any combined lateral-directional oscillations (‘Dutch roll’) occurring between 1·13 VSR and maximum allowable speed appropriate to the configuration of the aeroplane must be positively damped with controls free, and must be controllable with normal use of the primary controls without requiring exceptional pilot skill.

IR · CS 25.181 — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

AMCAcceptable means of compliance

AMC 25.181Dynamic stability

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The requirements of CS 25.181 are applicable at all speeds between the stalling speed and VFE, VLE or VFC/MFC, as appropriate.

AMC · AMC 25.181 — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

All rules in SUBPART B – FLIGHT

Consolidated from the EASA Easy Access Rules (revision 26 Jan 2023, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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