AEROELASTIC STABILITY SUBSTANTIATION OF TRANSPORT CATEGORY AIRPLANES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2014

Publisher

Federal Aviation Administration

1 Purpose
2 Applicability
3 Cancellation
4 Related 14 CFR Regulations
5 Background
6 Discussion of Requirements
7 Compliance

Specifies guidance material for acceptable means, but not the only means, of demonstrating compliance with the provisions of Title 14, Code of Federal Regulations (14 CFR) part 25 associated with the design requirements for transport category airplanes to preclude the aeroelastic instabilities of flutter, divergence, and control reversal.

DocumentType	Standard
Pages	23
PublisherName	Federal Aviation Administration
Status	Current

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