CS 22.351 Yawing conditions

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ED Decision 2003/13/RM

The sailplane must be designed for yawing loads on the vertical tail surface specified in CS 22.441 and CS 22.443.

Source-Title: CS 22.351 Yawing conditions View latest amendments

Erulesid: ERULES-1963177438-5339 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