NSN 9535-01-531-7061 of Sheet Metal - Parts Details
Alternative NSN: 9535015317061 |
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: 015317061 |
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 4, AMS-QQ-A-250 4-CD0-0 05X6X36, AMS-QQ-A-250 4-O-0.050X6X36 under NSN 9535-01-531-7061 of Sheet Metal manufactured by Sae International, Society Of Automotive Engineers Inc.
Federal Supply Class of NSN 9535-01-531-7061 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 9535-01-531-7061, 9535015317061
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Part No Manufacturer Item Name QTY 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 AMS-QQ-A-250 4-CD0-0 05X6X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 4-O-0.050X6X36 Sae International sheet metal Avl RFQ AMS-QQ-A-250 4-O-0.050X6X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ
Characteristics Data of NSN 9535015317061MRC Criteria Characteristic MDCL Material Document And Classification QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE HEAT Heat Treatment O-ANNEALED AGTA Basic Shape Style SOLID ABRY Length 36.000 INCHES NOMINAL FEAT Special Features MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH AGAV End Item Identification FUSELAGE F4F JET AIRCRAFT MRC Decoded Requirement Clear Text Reply ABGL Width 6.000 INCHES NOMINAL ALBY Usage Design AIRCRAFT MATT Material ALUMINUM ALLOY 2024 AARN Fabrication Method ROLLED ADVM Cross-Sectional Thickness 0.0500 INCHES NOMINAL
MRC | Criteria | Characteristic |
---|---|---|
MDCL | Material Document And Classification | QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE |
HEAT | Heat Treatment | O-ANNEALED |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
FEAT | Special Features | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
MRC | Decoded Requirement | Clear Text Reply |
ABGL | Width | 6.000 INCHES NOMINAL |
ALBY | Usage Design | AIRCRAFT |
MATT | Material | ALUMINUM ALLOY 2024 |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0500 INCHES NOMINAL |