The material will be applicable to Part 23 aircraft structural assessments at all levels (Levels 1 through 4), and is specifically related to damage tolerance evaluations for composite structure identified by ASTM F3115.
damage tolerance; durability; composite; aircraft; carbon fiber laminate; composite repair
Material will be provided to assist users of ASTM F3115 when performing damage tolerance evaluations identified in F3115. The material is specific to aircraft composite structure damage tolerance evaluations, and is considered a companion to another ASTM Practice workgroup for General Damage Tolerance Evaluations.
The title and scope are in draft form and are under development within this ASTM Committee.
Date Initiated: 05-17-2023
Technical Contact: Jay Yeakle