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National Stock Number:
9535-01-531-7792
Federal Supply Class:
9535
National Item Identification Number:
015317792
Description:
SHEET,METAL
Detail:
A FERROUS OR NONFERROUS PRODUCT WITH CROSS-SECTIONAL DIMENSIONS LIMITED TO THOSE ESTABLISHED IN APPENDIX C, FIIG A131. INCLUDES CORRUGATED AND PERFORATED ITEMS. FOR ITEMS 0.005 INCH OR .125MM THICK AND LESS. SEE FOIL, METAL. FOR SILVER ITEMS SEE SILVER SHEET.
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Manufacturer Information:
| AMS-QQ-A-250/5 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-250/5 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-250/5-CDT3-0,08X12X24 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-250/5-T3-0.080X12X24 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-250/5-T3-0.080X12X24 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
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Techincal Specification:
| BASIC SHAPE STYLE | SOLID | | CROSS-SECTIONAL THICKNESS | 0.0800 INCHES NOMINAL | | FABRICATION METHOD | ROLLED | | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED | | LENGTH | 24.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH | | MINIMUM YIELD STRENGTH | 40000 POUNDS PER SQUARE INCH | | SPECIAL FEATURES | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS | | WIDTH | 12.000 INCHES NOMINAL | | USAGE DESIGN | AIRCRAFT |
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