NSN 9535-01-531-2532 of Sheet Metal - Parts Details
| Alternative NSN: 9535015312532 |
| 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: 015312532 |
| NCB Code: USA (01) |
| Manufacturers: Society Of Automotive Engineers Inc , Sae International |
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 11-T0-0.063X12X48, QQ A 250 11 T0 0 063X12X48, AMS-QQ-A-250 11-CD0-0 063X12X48 under NSN 9535-01-531-2532 of Sheet Metal manufactured by Society Of Automotive Engineers Inc, Sae International.
Federal Supply Class of NSN 9535-01-531-2532 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 9535-01-531-2532, 9535015312532
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Part No Manufacturer Item Name QTY RFQ QQ-A-250 11-T0-0.063X12X48 Society Of Automotive Engineers Inc sheet metal Avl RFQ QQ A 250 11 T0 0 063X12X48 Sae International sheet metal Avl RFQ AMS-QQ-A-250 11-CD0-0 063X12X48 Society Of Automotive Engineers Inc sheet metal Avl RFQ
Characteristics Data of NSN 9535015312532MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ABGL WIDTH 12.000 INCHES NOMINAL ABRY LENGTH 48.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.0630 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE, F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID MATL MATERIAL ALUMINUM ALLOY, AMS-Q-250/11, ALLOY 6061 AARN FABRICATION METHOD ROLLED ABGL WIDTH 12.000 INCHES NOMINAL ABRY LENGTH 48.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.0630 INCHES NOMINAL AGAV END ITEM IDENTIFICATION FUSELAGE, F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID MATL MATERIAL ALUMINUM ALLOY, AMS-Q-250/11, ALLOY 6061
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE, F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| MATL | MATERIAL | ALUMINUM ALLOY, AMS-Q-250/11, ALLOY 6061 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE, F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| MATL | MATERIAL | ALUMINUM ALLOY, AMS-Q-250/11, ALLOY 6061 |