Part Number List of NSN 9535-01-531-7794, 9535015317794 - Sheet Metal
The NSN part number 9535-01-531-7794 manufactured by Society Of Automotive Engineers Inc, Sae International is available in NSN Components’ inventory. Owned and operated by ASAP Semiconductor, we have an inventory of over six billion parts, including NSN Parts AMS-QQ-A-250 5-CDT3-0 08X6X36, AMS-QQ-A-250 5, AMS QQ A 250 5 T3 0 080X6X36, AMS QQ A 250 5 T3 0 080X6X36, AMS QQ A 250 5. ASAP is dedicated to streamlining the parts procurement process for our customers, with dedicated account managers ready to solve procurement issues that they face. Each NSN 9535-01-531-7794 part of Sheet Metal we ship goes through numerous quality checks and inspections, to ensure we sell only the highest-quality parts. Ready to start? Then submit a Request for Quote from this page today.
| Alternative NSN: 9535-01-531-7794 |
| Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
| NIIN: 015317794 |
| NCB Code: USA (01) |
| Manufacturers: Sae International, Society Of Automotive Engineers Inc |
Part Number's List for NSN 9535-01-531-7794, 9535015317794
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 5-CDT3-0 08X6X36 | 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 080X6X36 | sae international | sheet metal | Avl | RFQ |
| AMS QQ A 250 5 T3 0 080X6X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
| AMS QQ A 250 5 | sae international | sheet metal | Avl | RFQ |
Product Characteristics of NSN 9535015317794
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0800 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 | 61000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 40000 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 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 |
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