Fatigue, fail-safe, and damage tolerance evaluation of metallic structure for normal, utility, acrobatic, and commuter category airplanes.

Bibliographic Details
Corporate Author: United States. Federal Aviation Administration
Format: Government Document Book
Language:English
Published: Washington, DC : U.S. Dept. of Transportation, Federal Aviation Administration : [2005]
Series:Advisory circular ; AC 23-13A
Subjects:
Online Access:https://purl.fdlp.gov/GPO/LPS105323

Internet

https://purl.fdlp.gov/GPO/LPS105323

Available Online

Holdings details from Available Online
Call Number: TD 4.8/5:23-13 A
 
Call Number Status Get It
TD 4.8/5:23-13 A Available