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CS-VLA 641  Proof of strength

ED Decision 2003/18/RM

The strength of stressed-skin wings must be proven by load tests or by combined structural analysis and load tests.
Details
Source-Title: CS-VLA 641 Proof of strength View latest amendments
Erulesid: ERULES-1963177438-7856 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