Browse NSN 9535-01-531-7798 Listing of Sheet 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-CDT3-0 071X12X48, AMS QQ A 250 5 T3 0 071X12X48, AMS QQ A 250 5 T3 0 071X12X48 listed under NSN 9535-01-531-7798 is now available and ready to ship from Fulfillment By ASAP. This part described as a Sheet Metal manufactured by Society Of Automotive Engineers Inc, Sae Inc. If you’d like a quick quote for NSN 9535-01-531-7798, 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: 9535-01-531-7798 |
Item Name: Sheet Metal |
Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NIIN: 015317798 |
NCB Code: USA (01) |
Manufacturers: Sae Inc , Society Of Automotive Engineers Inc |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
AMS QQ A 250 5 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5 | sae inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5-CDT3-0 071X12X48 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS QQ A 250 5 T3 0 071X12X48 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS QQ A 250 5 T3 0 071X12X48 | sae inc | sheet metal | Avl | RFQ |
Characteristics Data of NSN 9535015317798
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 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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