CS 22.441 Manoeuvring loads

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ED Decision 2003/13/RM

The vertical tail surfaces must be designed for manoeuvring loads imposed by the following conditions:

(a) At speed the greater of V_A and V_T, full deflection of the rudder.

(b) At speed V_D, one-third of full deflection of the rudder.

Source-Title: CS 22.441 Manoeuvring loads View latest amendments

Erulesid: ERULES-1963177438-5355 Compare versions

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 14 November, 2003

Entryintoforcedate: 14 November, 2003

Regulatorysource: ED Decision 2003/13/RM Navigate

Regulatorysubject: CS-22

Typeofcontent: CS (Certification specification)

Origin: EASA

Category: EAR