NSN 9535-01-531-7787 of Sheet Metal - Product Details
Just NSN Parts, owned and operated by ASAP Semiconductor, is an industry-leading distributor of NSN 9535-01-531-7787 parts applicable in the aviation and defense industries. We aim to simplify the NSN 9535-01-531-7787 parts procurement process by enabling our customers to search through our inventory quickly and efficiently. Type in your desired NSN 9535-01-531-7787 part number such as AMS-QQ-A-250 5-T3-0.025X6X36, AMS-QQ-A-250 5, AMS QQ A 250 5 T3 0 025X6X36, AMS QQ A 250 5 CDT3 0 025X6X36 into our search engine and, in a matter of seconds, available stock will appear.
We pride ourselves on our attention to detail and focus on quality control. We are FAA AC 0056B accredited and AS9120B, ISO 9001:2015 certified. We offer our customers a personalized and reliable service that will change your parts procurement process. If you would like to receive a quote today, fill out a request for quote form today.
Alternative NSN: 9535-01-531-7787 |
Item Name:Sheet Metal |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NIIN: 015317787 |
NCB Code: USA (01) |
Manufacturers: Society Of Automotive Engineers Inc , Sae International |
Manufacturer's List for NSN 9535-01-531-7787, 9535015317787
Part Number Related To NSN 9535-01-531-7787, 9535015317787
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
AMS-QQ-A-250 5-T3-0.025X6X36 | 9535-01-531-7787 | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5 | 9535-01-531-7787 | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5 | 9535-01-531-7787 | sheet metal | Avl | RFQ |
AMS QQ A 250 5 T3 0 025X6X36 | 9535-01-531-7787 | sheet metal | Avl | RFQ |
AMS QQ A 250 5 CDT3 0 025X6X36 | 9535-01-531-7787 | sheet metal | Avl | RFQ |
Characteristics Data of NSN 9535015317787
MRC | Criteria | Characteristic |
---|---|---|
ADVM | CROSS-SECTIONAL THICKNESS | 0.0250 INCHES NOMINAL |
ALBY | III USAGE DESIGN | AIRCRAFT |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 39000 POUNDS PER SQUARE INCH |
AARN | FABRICATION METHOD | ROLLED |
FEAT | 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
AGTA | BASIC SHAPE STYLE | SOLID |
ABRY | LENGTH | 36.000 INCHES NOMINAL |