9535-01-531-7794 SHEET,METAL Index 9535-01-531-7796 SHEET,METAL

National Stock Number:
9535-01-531-7795

Federal Supply Class:
9535

National Item Identification Number:
015317795

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.


Manufacturer Information:
AMS-QQ-A-250/50U583SAE INTERNATIONAL
AMS-QQ-A-250/581343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-250/5-CDT81-0,04X12X3681343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-250/5-T81-0.040X12X360U583SAE INTERNATIONAL
AMS-QQ-A-250/5-T81-0.040X12X3681343SOCIETY OF AUTOMOTIVE ENGINEERS INC


Techincal Specification:
BASIC SHAPE STYLESOLID
CROSS-SECTIONAL THICKNESS0.0400 INCHES NOMINAL
FABRICATION METHODROLLED
HEAT TREATMENTT-81 SOLUTION HEAT TREATED
LENGTH36.000 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
MINIMUM TENSILE STRENGTH62000 POUNDS PER SQUARE INCH
MINIMUM YIELD STRENGTH54000 POUNDS PER SQUARE INCH
SPECIAL FEATURESTHIN 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS
WIDTH12.000 INCHES NOMINAL
USAGE DESIGNAIRCRAFT


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