CS 25.333 Flight manoeuvring envelope

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

IRImplementing rule

CS 25.333Flight manoeuvring envelope

(See AMC 25.333)

(a)General. The strength requirements must be met at each combination of airspeed and load factor on and within the boundaries of the representative manoeuvring envelope (V-n diagram) of sub-paragraph (b) of this paragraph. This envelope must also be used in determining the aeroplane structural operating limitations as specified in CS 25.1501.

(b)Manoeuvring envelope (See AMC 25.333(b)) [Figure or form omitted from this preview — available in the Avioverse workspace library.]

[Amdt 25/11]

[Amdt 25/13]

[Amdt 25/18]

IR · CS 25.333 — CS-25 · ED Decision 2016/010/R · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

AMCAcceptable means of compliance

AMC 25.333(b)Manoeuvring envelope

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For the calculation of structural design speeds, the stalling speeds Vs0 and Vs1 should be taken to be the 1-g stalling speeds in the appropriate flap configuration. This structural interpretation of stalling speed should be used in connection with the paragraphs CS 25.333(b), CS 25.335, CS 25.335(c)(d)(e), CS 25.479(a), and CS 25.481(a)(1).

[Amdt 25/13]

AMC · AMC 25.333(b) — CS-25 · ED Decision 2013/010/R · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

All rules in SUBPART C – STRUCTURE

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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