CS 31GB.44 Protection of envelope against tearing

ED Decision 2011/012/R

The design of the envelope must be such that, while supporting limit load, local damage will not grow to an extent that results in uncontrolled flight or landing.

Table of Contents Ask question Discover more

AI for Aviation Professionals

Aviation.Bot is an AI tool that assists you with aviation compliance.

Details

Source-Title: CS 31GB.44 Protection of envelope against tearing

Erulesid: ERULES-1963177438-4519

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 12 December, 2011

Entryintoforcedate: 12 December, 2011

Regulatorysource: ED Decision 2011/012/R Navigate

Regulatorysubject: CS-31GB

Typeofcontent: CS (Certification specification)

Origin: EASA

Category: EAR

Navigate / EASA / CS 31GB I1 / SUBPART D -- DESIGN AND CONSTRUCTION /

CS 31GB.44 Protection of envelope against tearing

Related

AI for Aviation Professionals

Details