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CS-VLA 351  Yawing conditions

ED Decision 2003/18/RM

The aeroplane must be designed for yawing loads on the vertical tail surfaces resulting from the loads specified in CS-VLA 441 to 445.

Details
Source-Title: CS-VLA 351 Yawing conditions View latest amendments
Erulesid: ERULES-1963177438-8059 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 14 November, 2003
Entryintoforcedate: 14 November, 2003
Regulatorysource: ED Decision 2003/18/RM Navigate
Regulatorysubject: CS-VLA
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR