Navigate / EASA
Ask question Discover more Add to collection

AMC VLA 572(a)  Parts of structure critical to safety (Interpretative Material)

ED Decision 2003/18/RM

At least the wing main spar, the horizontal tail and their attachments to the fuselage should be investigated to determine whether or not their stress levels exceed the values given in the table in AMC VLA 572(b).
Details
Source-Title: AMC VLA 572(a) Parts of structure critical to safety (Interpretative Material) View latest amendments
Erulesid: ERULES-1963177438-7890 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: AMC to CS (Acceptable means of compliance to certification specification)
Origin: EASA
Category: EAR