NSN 9535-01-531-6273

Part Details | METAL SHEET

9535-01-531-6273 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.

Alternate Parts: AMSQQA2504CDT30,19X12X48, AMS-QQ-A-250/4-CDT3-0,19X12X48, AMSQQA2504, AMS-QQ-A-250/4, AMSQQA2504AT30120X0480X0.1900, AMSQQA250/4AT3-0120X0480X0.1900, AMSQQA2504AT348.0X12.0X0.190, AMSQQA250/4A-T3-48.0X12.0X0.190, AMSQQA2504T30.190X12X48, AMS-QQ-A-250/4-T3-0.190X12X48, 9535-01-531-6273, 01-531-6273, 9535015316273, 015316273

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JUL 15, 200501-531-627337015 ( SHEET, METAL )
REFERENCE DRAWINGS & PICTURES

ROUND

Cross Reference | NSN 9535-01-531-6273
Part Number Cage Code Manufacturer
AMS-QQ-A-250/4-CDT3-0,19X12X4881343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-250/481343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMSQQA250/4AT3-0120X0480X0.190081343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMSQQA250/4A-T3-48.0X12.0X0.19081343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-250/4-T3-0.190X12X4881343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 9535-01-531-6273
Characteristic Specifications
MATERIAL ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250 TO 4 FED SPEC SINGLE MATERIAL RESPONSE
FABRICATION METHODS ANY ACCEPTABLE
HEAT TREATMENT T-3 SOLUTION HEAT TREATED
MINIMUM TENSILE STRENGTH64000 POUNDS PER SQUARE INCH
MINIMUM YIELD STRENGTH42000 POUNDS PER SQUARE INCH
LENGTH48.000 INCHES NOMINAL
BASIC SHAPE STYLE0 ROUND
WIDTH12.000 INCHES NOMINAL
CROSS-SECTIONAL THICKNESS0.1900 INCHES NOMINAL
PHYSICAL FORM FLAT STOCK
SPECIFICATION/STANDARD DATA81343-SAE-AMS-QQ-A-250 TO 4A NATIONAL STD/SPEC
USAGE DESIGN AIRCRAFT
END ITEM IDENTIFICATIONFUSELAGE F4F JET AIRCRAFT
PART NAME ASSIGNED BY CONTROLLING AGENCYALUMINUM ALLOY 2024,PLATE AND SHEET