NSN 9535-01-531-7078 of Sheet Metal - Parts Details
| Alternative NSN: 9535015317078 |
| 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: 015317078 |
| 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 AMS-QQ-A-250 4-O0.125X12X48, AMS-QQ-A-250 4-CD0-0 125X12X48, AMS-QQ-A-250 4 under NSN 9535-01-531-7078 of Sheet Metal manufactured by Society Of Automotive Engineers Inc, Sae International.
Federal Supply Class of NSN 9535-01-531-7078 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 9535-01-531-7078, 9535015317078
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Part No Manufacturer Item Name QTY RFQ AMS-QQ-A-250 4-O0.125X12X48 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 4-O0.125X12X48 Sae International sheet metal Avl RFQ AMS-QQ-A-250 4-CD0-0 125X12X48 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 4 Sae International sheet metal Avl RFQ AMS-QQ-A-250 4 Society Of Automotive Engineers Inc sheet metal Avl RFQ
Characteristics Data of NSN 9535015317078MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ABGL WIDTH 12.000 INCHES NOMINAL ABRY LENGTH 48.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.1250 INCHES NOMINAL AGAV III END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID ALBY III USAGE DESIGN AIRCRAFT FEAT SPECIAL FEATURES MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH HEAT HEAT TREATMENT O-ANNEALED MATT MATERIAL ALUMINUM ALLOY 2024 MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.1250 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | III USAGE DESIGN | AIRCRAFT |
| FEAT | SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |