NSN 9535-01-531-2515 of Sheet Metal - Parts Details
| Alternative NSN: 9535015312515 |
| 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: 015312515 |
| NCB Code: USA (01) |
| Manufacturers: Sae International , Society Of Automotive Engineers Inc |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers QQ-A-250 1-H14-0.032X12X48, AMS QQ A 250 1 CDH14 0 032X12X48 under NSN 9535-01-531-2515 of Sheet Metal manufactured by Sae International, Society Of Automotive Engineers Inc.
Federal Supply Class of NSN 9535-01-531-2515 is FSC 9535 contains part details of Plate Sheet Strip and Foil Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9535-01-531-2515, 9535015312515
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Part No Manufacturer Item Name QTY RFQ QQ-A-250 1-H14-0.032X12X48 Sae International sheet metal Avl RFQ QQ-A-250 1-H14-0.032X12X48 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS QQ A 250 1 CDH14 0 032X12X48 Society Of Automotive Engineers Inc sheet metal Avl RFQ
Characteristics Data of NSN 9535015312515MRC Criteria Characteristic CQHQ Minimum Yield Strength 14000 POUNDS PER SQUARE INCH AGTA Basic Shape Style SOLID MRC Decoded Requirement Clear Text Reply ABRY Length 48.000 INCHES NOMINAL ABGL Width 12.000 INCHES NOMINAL AGAV End Item Identification FUSELAGE F4F JET AIRCRAFT CQBC Minimum Tensile Strength 16000 POUNDS PER SQUARE INCH MATT Material ALUMINUM ALLOY 1100 AARN Fabrication Method ROLLED MDCL Material Document And Classification QQ-A-250/1 FED SPEC 1ST MATERIAL RESPONSE ADVM Cross-Sectional Thickness 0.0320 INCHES NOMINAL
| MRC | Criteria | Characteristic |
|---|---|---|
| CQHQ | Minimum Yield Strength | 14000 POUNDS PER SQUARE INCH |
| AGTA | Basic Shape Style | SOLID |
| MRC | Decoded Requirement | Clear Text Reply |
| ABRY | Length | 48.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| CQBC | Minimum Tensile Strength | 16000 POUNDS PER SQUARE INCH |
| MATT | Material | ALUMINUM ALLOY 1100 |
| AARN | Fabrication Method | ROLLED |
| MDCL | Material Document And Classification | QQ-A-250/1 FED SPEC 1ST MATERIAL RESPONSE |
| ADVM | Cross-Sectional Thickness | 0.0320 INCHES NOMINAL |