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.

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Source-Title: AMC 31HB.28(c) Tethered flight loads

Erulesid: ERULES-1963177438-5009

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)

Origin: EASA

Category: EAR