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AMC1 LSA.5  Applicability

ED Decision 2011/005/R

This CS-LSA is applicable to aeroplanes that are by definition engine-driven by design and therefore this CS-LSA is not applicable to powered sailplanes that are designed for sailplane characteristics when the engine is inoperative.
Details
Source-Title: AMC1 LSA.5 Applicability View latest amendments
Erulesid: ERULES-1963177438-7033 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 4 July, 2011
Entryintoforcedate: 4 July, 2011
Regulatorysource: ED Decision 2011/005/R Navigate
Regulatorysubject: CS-LSA
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS-LSA.5 Applicability
Origin: EASA
Category: EAR