NSN 9535-01-531-7789 of Sheet Metal - Parts Details
| Alternative NSN: 9535015317789 |
| 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: 015317789 |
| 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 5-T3-0.040X6X36, AMS-QQ-A-250 5-CDT3-0 04X6X36, AMS-QQ-A-250 5, AMS QQ A 250 5 T3 0 040X6X36, AMS QQ A 250 5 under NSN 9535-01-531-7789 of Sheet Metal manufactured by Society Of Automotive Engineers Inc, Sae International.
Federal Supply Class of NSN 9535-01-531-7789 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 9535-01-531-7789, 9535015317789
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Part No Manufacturer Item Name QTY RFQ AMS-QQ-A-250 5-T3-0.040X6X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 5-CDT3-0 04X6X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 5 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS QQ A 250 5 T3 0 040X6X36 Sae International sheet metal Avl RFQ AMS QQ A 250 5 Sae International sheet metal Avl RFQ
Characteristics Data of NSN 9535015317789MRC Criteria Characteristic MATT Material ALUMINUM ALLOY 2024 MDCL Material Document And Classification QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE CQHQ Minimum Yield Strength 39000 POUNDS PER SQUARE INCH AGTA Basic Shape Style SOLID ABRY Length 36.000 INCHES NOMINAL HEAT Heat Treatment T-3 SOLUTION HEAT TREATED AGAV End Item Identification FUSELAGE F4F JET AIRCRAFT ABGL Width 6.000 INCHES NOMINAL CQBC Minimum Tensile Strength 59000 POUNDS PER SQUARE INCH MRC Decoded Requirement Clear Text Reply ALBY Usage Design AIRCRAFT FEAT Special Features THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS AARN Fabrication Method ROLLED ADVM Cross-Sectional Thickness 0.0400 INCHES NOMINAL
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | Material | ALUMINUM ALLOY 2024 |
| MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
| CQHQ | Minimum Yield Strength | 39000 POUNDS PER SQUARE INCH |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 36.000 INCHES NOMINAL |
| HEAT | Heat Treatment | T-3 SOLUTION HEAT TREATED |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| ABGL | Width | 6.000 INCHES NOMINAL |
| CQBC | Minimum Tensile Strength | 59000 POUNDS PER SQUARE INCH |
| MRC | Decoded Requirement | Clear Text Reply |
| ALBY | Usage Design | AIRCRAFT |
| FEAT | Special Features | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |