NSN 9535-01-532-0507 of Sheet Metal - Parts Details
| Alternative NSN: 9535015320507 |
| 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: 015320507 |
| 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 AMS-QQ-A-250 8-H34-0.020X12X36, AMS-QQ-A-250 8-CDH34-0 02X12X36, AMS-QQ-A-250 8 under NSN 9535-01-532-0507 of Sheet Metal manufactured by Sae International, Society Of Automotive Engineers Inc.
Federal Supply Class of NSN 9535-01-532-0507 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 9535-01-532-0507, 9535015320507
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Part No Manufacturer Item Name QTY RFQ AMS-QQ-A-250 8-H34-0.020X12X36 Sae International sheet metal Avl RFQ AMS-QQ-A-250 8-H34-0.020X12X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 8-CDH34-0 02X12X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 8 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 8 Sae International sheet metal Avl RFQ
Characteristics Data of NSN 9535015320507MRC Criteria Characteristic MATT Material ALUMINUM ALLOY 5052 HEAT Heat Treatment H-34 STRAIN HARDENED AGTA Basic Shape Style SOLID ABRY Length 36.000 INCHES NOMINAL ABGL Width 12.000 INCHES NOMINAL AGAV End Item Identification FUSELAGE, F4F JET AIRCRAFT CQBC Minimum Tensile Strength 34000 POUNDS PER SQUARE INCH MDCL Material Document And Classification QQ-A-250/8 FED SPEC 1ST MATERIAL RESPONSE ALBY Usage Design AIRCRAFT MRC Decoded Requirement Clear Text Reply FEAT Special Features MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH AARN Fabrication Method ROLLED ADVM Cross-Sectional Thickness 0.0200 INCHES NOMINAL
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | Material | ALUMINUM ALLOY 5052 |
| HEAT | Heat Treatment | H-34 STRAIN HARDENED |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 36.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE, F4F JET AIRCRAFT |
| CQBC | Minimum Tensile Strength | 34000 POUNDS PER SQUARE INCH |
| MDCL | Material Document And Classification | QQ-A-250/8 FED SPEC 1ST MATERIAL RESPONSE |
| ALBY | Usage Design | AIRCRAFT |
| MRC | Decoded Requirement | Clear Text Reply |
| FEAT | Special Features | MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.0200 INCHES NOMINAL |