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National Stock Number:
9535-01-531-7800
Federal Supply Class:
9535
National Item Identification Number:
015317800
Description:
PLATE,METAL
Detail:
A ferrous or nonferrous product with cross-sectional dimensions limited to those established in Appendix C, FIIG A131. Excludes ARMOR PLATE; PLATE, FLOOR, METAL; TERNEPLATE; and TINPLATE. For silver plate 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-CDT351-1,0X6X24 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-QQ-A-250/5-T351-1.000X6X24 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-250/5-T351-1.000X6X24 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
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Techincal Specification:
| BASIC SHAPE STYLE | SOLID | | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL | | FABRICATION METHOD | ROLLED | | HEAT TREATMENT | T-351 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 | 62000 POUNDS PER SQUARE INCH | | MINIMUM YIELD STRENGTH | 42000 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 PLATE THICKNESS | | WIDTH | 6.000 INCHES NOMINAL | | USAGE DESIGN | AIRCRAFT |
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