Inactive Total Small Business Set-Aside (FAR 19.5)

Parts shall be fabricated per drawings X202405988 and X202405989 using fiberglass material to a thickness of 1/ 16 inch. This order calls for (2) EA of both part designs. Approval from cognizant engin... Parts shall be fabricated per drawings X202405988 and X202405989 using fiberglass material to a thickness of 1/ 16 inch. This order calls for (2) EA of both part designs. Approval from cognizant engineering authority shall be obtained on the completed mold dimensions before proceeding with fiberglass layup. The contractor shall provide documentation of materials used, manufacturing processes, and any certificates relevant to the final product. All drawings and designs related to this order are the sole property of the United States Air Force, and may not be distributed, replicated, or otherwise reproduced without prior consent from the owning organization.