NSN - 9535-01-531-7800, 9535015317800 of Plate Metal
Aviation Axis stocks AMS-QQ-A-250 5, AMS QQ A 250 5, AMS-QQ-A-250 5-CDT351-1 0X6X24, AMS-QQ-A-250 5-T351-1.000X6X24 - Plate Metal made by Sae International, Society Of Automotive Engineers Inc with 9535-01-531-7800. Owned and operated by ASAP Semiconductor, we have access to over 2 billion new and after-market parts applicable within the aerospace and defense industries. All our parts are shipped using our premier shipping and supply chain. We offer short lead-times and some of the fastest shipping times in the industry. We are well-equipped to handle any customer situation - including AOG. Submit an RFQ today and expect a response within 15 minutes or less. ASAP - the evolution of purchasing.
| Alternative NSN: 9535-01-531-7800 |
| Item Name: Plate Metal |
| Federal Supply Class (FSC): 9535 Plate Sheet Strip And Foil Nonferrous Base Metal |
| NIIN: 015317800 |
| NCB Code: USA (01) |
| Manufacturers: Sae International, Society Of Automotive Engineers Inc |
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 5 | sae international | plate metal | Avl | RFQ |
| AMS QQ A 250 5 | society of automotive engineers inc | plate metal | Avl | RFQ |
| AMS-QQ-A-250 5-CDT351-1 0X6X24 | society of automotive engineers inc | plate metal | Avl | RFQ |
| AMS-QQ-A-250 5-T351-1.000X6X24 | society of automotive engineers inc | plate metal | Avl | RFQ |
| AMS-QQ-A-250 5-T351-1.000X6X24 | sae international | plate metal | Avl | RFQ |
Technical Characteristics of NSN 9535015317800
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 24.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 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 | 62000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 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 PLATE THICKNESS |
| HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
Related NSN List for 9535-01-531-7800, 9535015317800
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