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AMC 31HB.28(c) Tethered flight loads

ED Decision 2009/005/R

An appropriate factor of safety is CS 31HB.25(a) for metallic components or CS 31HB.25(c) for non-metallic or fibrous suspension components.
Details
Source-Title: AMC 31HB.28(c) Tethered flight loads View latest amendments
Erulesid: ERULES-1963177438-5009 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 5 March, 2009
Entryintoforcedate: 5 March, 2009
Regulatorysource: ED Decision 2009/005/R Navigate
Regulatorysubject: CS-31HB
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS 31HB.28 Tethered flight loads
Origin: EASA
Category: EAR