Name: FAA AC 25.613-1 : 2003
Brand: FAA

MATERIAL STRENGTH PROPERTIES AND MATERIAL DESIGN VALUES

Published date

12-01-2013

Publisher

Federal Aviation Administration

1. PURPOSE
2. APPLICABILITY
3. RELATED FAR SECTIONS
4. RELATED ADVISORY CIRCULARS
5. DEFINITIONS
6. BACKGROUND
7. DISCUSSION

Gives guidance for demonstrating compliance with the airworthiness standards that specify the requirements for material strength properties and material design values. This guidance is applicable to transport category airplanes for which a new, amended, or supplemental type certificate is requested.

DocumentType	Standard
PublisherName	Federal Aviation Administration
Status	Current

SAE ARP 4058 : 2017

GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS

FAA AC 20-107 : 2009	COMPOSITE AIRCRAFT STRUCTURE
FAA AC 25.571-1 : 2011	DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE

View more information

Sorry this product is not available in your region.

Access your standards online with a subscription

Features

Simple online access to standards, technical information and regulations.
Critical updates of standards and customisable alerts and notifications.
Multi-user online standards collection: secure, flexible and cost effective.

Learn more on subscription solutions

Get in touch with us

Log into your Account

FAA AC 25.613-1 : 2003

Current

Table of Contents

Abstract

General Product Information

Standards Referenced By This Book

Standards Referencing This Book

Category

Subcategory

Access your standards online with a subscription