NSN 9535-01-531-7806, 9535015317806 Sheet Metal Parts Sourcing
If you have been looking for Society Of Automotive Engineers Inc, Sae International parts listed alongside the NSN 9535015317806, ASAP Distribution has you covered with our unmatched inventory of items Sheet Metal. With over 2 billion parts readily available for purchase on our website, customers can get competitive pricing offers and rapid lead-times on top NSN part numbers such as AMS-QQ-A-250 5, AMS-QQ-A-250 5-T81-0.080X12X48, AMS-QQ-A-250 5-CDT81-0 08X12X48. Explore our NSN parts catalog at your leisure, or you may take advantage of our provided search engine to find specific parts in a matter of moments. If you are interested in this particular component or others listed across our website, you may begin the procurement process at any time through the submission of an Instant RFQ form. Using the information that you submit to us, our team of industry experts will quickly craft you a quote that accommodates your individual needs and requirements for NSN 9535015317806.
| Alternative NSN: 9535-01-531-7806 | 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: 015317806 | NCB Code: USA (01) |
Part Number's List for NSN 9535-01-531-7806, 9535015317806
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 5 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-T81-0.080X12X48 | Sae International | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-T81-0.080X12X48 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5 | Sae International | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-CDT81-0 08X12X48 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
Characteristics Data of NSN 9535015317806
| MRC | Criteria | Characteristic |
|---|---|---|
| ALBY | III USAGE DESIGN | AIRCRAFT |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0800 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 65000 POUNDS PER SQUARE INCH |
| AARN | FABRICATION METHOD | ROLLED |
| CQHQ | MINIMUM YIELD STRENGTH | 56000 POUNDS PER SQUARE INCH |
| 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
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