1.1 This specification addresses structural durability for small airplanes. 1.2 This specification provides an acceptable means of compliance to 14 CFR Part 23, 23.571. 1.3 This specification applies to any structure the failure of which could result in large reductions in safety margins or functional capabilities, serious or fatal injuries, or loss of the airplane. 1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
Keywordsstructure; fatigue loading; general aviation; aircraft
The title and scope are in draft form and are under development within this ASTM Committee.Back to Top
Withdrawn From Balloting
Ballot Item Approved as F3115-2015 and Pending Publication