Browse NSN 9535-01-531-7800 Listing of Plate Metal
It is our pleasure to inform you that part number 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, AMS QQ A 250 5 T351 1 000X6X24 listed under NSN 9535-01-531-7800 is now available and ready to ship from Fulfillment By ASAP. This part described as a Plate Metal manufactured by Sae Inc, Society Of Automotive Engineers Inc. If you’d like a quick quote for NSN 9535-01-531-7800, please fill out the form from below. Are you looking to have it delivered today or tomorrow? We can help! Simply complete the Request For Quote (RFQ) form given below to get started, and we will get back to you within 15 minutes!
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 Inc , Society Of Automotive Engineers Inc |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
AMS QQ A 250 5 | sae inc | 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 inc | plate metal | Avl | RFQ |
Characteristics Data 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 |
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