NSN 9535-01-531-7784 of Sheet Metal - Parts Details
| Alternative NSN: 9535015317784 |
| 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: 015317784 |
| 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-T3-0.040X12X36, AMS-QQ-A-250 5, AMS QQ A 250 5 CDT3 0 04X12X36 under NSN 9535-01-531-7784 of Sheet Metal manufactured by Society Of Automotive Engineers Inc, Sae International.
Federal Supply Class of NSN 9535-01-531-7784 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 9535-01-531-7784, 9535015317784
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Part No Manufacturer Item Name QTY RFQ AMS-QQ-A-250 5-T3-0.040X12X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS-QQ-A-250 5-T3-0.040X12X36 Sae International sheet metal Avl RFQ AMS-QQ-A-250 5 Sae International sheet metal Avl RFQ AMS-QQ-A-250 5 Society Of Automotive Engineers Inc sheet metal Avl RFQ AMS QQ A 250 5 CDT3 0 04X12X36 Society Of Automotive Engineers Inc sheet metal Avl RFQ
Characteristics Data of NSN 9535015317784MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ABGL WIDTH 12.000 INCHES NOMINAL ABRY LENGTH 36.000 INCHES NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.0400 INCHES NOMINAL AGAV III END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT AGTA BASIC SHAPE STYLE SOLID ALBY III USAGE DESIGN AIRCRAFT CQBC MINIMUM TENSILE STRENGTH 59000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 39000 POUNDS PER SQUARE INCH 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 HEAT HEAT TREATMENT T-3 SOLUTION HEAT TREATED MATT MATERIAL ALUMINUM ALLOY 2024 MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | III USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 39000 POUNDS PER SQUARE INCH |
| 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 |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |