WK86457 - New Practice for General Damage Tolerance Evaluations

Work Item

ASTM WK86457

New Practice for General 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 structural damage tolerance evaluations identified by ASTM F3115.

Keywords

damage tolerance; durability; crack growth; structural fatigue; fatigue; stress spectra; load spectra; aircraft

Rationale

Material will be provided to assist users of ASTM F3115 when performing damage tolerance evaluations identified in F3115. The material is generalized to aircraft structural damage tolerance evaluations, and is applicable to both metallic and composite structures.

Details

Developed by Subcommittee: F44.30

Committee: F44

Staff Manager: Joe Koury

Work Item Status

Date Initiated: 05-17-2023

Technical Contact: A. K. M. Haque

Item: 002

Ballot: F44.30 (24-01)

Status: Will Reballot Item

Item: 004

Ballot: F44 (24-07)

Status: Ballot Item Approved