scope:

Use/Relationship: The report identifies the aircraft structure locations analyzed for durability and damage tolerance as required by MIL-STD-1530. The report details the assumptions, methods, procedures, and results of the airframe durability and damage tolerance analyses. The report also identifies inspection intervals and techniques necessary to detect damage growth in service. The report identifies the material quality and defines damage acceptance limits for honeycomb, bonded, and composite aircraft structures.

a. This Data Item Description (DID) contains the format and content preparation instructions for the data product generated by the specific and discrete task requirement as delineated in the contract.

b. This DID interfaces with DI-SESS-81485, Durability and Damage Tolerance (DADT) Test Report.

c. This DID supersedes DI-MISC-81486 and DI-MISC-81487. (Copies of these documents are available online at http://quicksearch.dla.mil.)