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CS-VLA 23  Load distribution limits

ED Decision 2003/18/RM

Ranges of weight and centres of gravity within which the aeroplane may be safely operated must be established and must include the range of lateral centres of gravity if possible loading conditions can result in significant variation of their positions.
Details
Source-Title: CS-VLA 23 Load distribution limits View latest amendments
Erulesid: ERULES-1963177438-8089 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