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National Stock Number:
9535-01-531-7062
Federal Supply Class:
9535
National Item Identification Number:
015317062
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-250/4 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-250/4 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-250/4-CD0-0,032X12X36 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-250/4-O-0.032X12X36 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-250/4-O-0.032X12X36 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
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Techincal Specification:
| BASIC SHAPE STYLE | SOLID | | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL | | FABRICATION METHOD | ROLLED | | HEAT TREATMENT | O-ANNEALED | | LENGTH | 36.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH | | WIDTH | 12.000 INCHES NOMINAL | | USAGE DESIGN | AIRCRAFT |
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