Work Item
ASTM WK86458

New Practice for Composite Damage Tolerance Evaluations

1. Scope

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.

Keywords

damage tolerance; durability; composite; aircraft; carbon fiber laminate; composite repair

Rationale

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.

Details

Developed by Subcommittee: F44.30

Committee: F44

Staff Manager: Joe Koury

Work Item Status

Date Initiated: 05-17-2023

Technical Contact: Jay Yeakle