Browse NSN 9535-01-531-7789 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 04X6X36, AMS QQ A 250 5 T3 0 040X6X36, AMS-QQ-A-250 5-T3-0.040X6X36 listed under NSN 9535-01-531-7789 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 9535-01-531-7789, 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: 9535-01-531-7789 |
Item Name: Sheet Metal |
Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NIIN: 015317789 |
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 04X6X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS QQ A 250 5 T3 0 040X6X36 | sae inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5-T3-0.040X6X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
Characteristics Data of NSN 9535015317789
MRC | Criteria | Characteristic |
---|---|---|
MATT | Material | ALUMINUM ALLOY 2024 |
MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
CQHQ | Minimum Yield Strength | 39000 POUNDS PER SQUARE INCH |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
HEAT | Heat Treatment | T-3 SOLUTION HEAT TREATED |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
ABGL | Width | 6.000 INCHES NOMINAL |
CQBC | Minimum Tensile Strength | 59000 POUNDS PER SQUARE INCH |
MRC | Decoded Requirement | Clear Text Reply |
ALBY | Usage Design | AIRCRAFT |
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 |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
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