Browse NSN 9535-01-532-0294 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 CD0 0 032X12X36, AMS-QQ-A-250 5-O-0.032X12X36, AMS QQ A 250 5 O 0 032X12X36 listed under NSN 9535-01-532-0294 is now available and ready to ship from Fulfillment By ASAP. This part described as a Sheet Metal manufactured by Sae Inc, Society Of Automotive Engineers Inc. If you’d like a quick quote for NSN 9535-01-532-0294, 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: 9535-01-532-0294 |
Item Name: Sheet Metal |
Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NIIN: 015320294 |
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 | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS QQ A 250 5 CD0 0 032X12X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5-O-0.032X12X36 | sae inc | sheet metal | Avl | RFQ |
AMS QQ A 250 5 O 0 032X12X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
Characteristics Data of NSN 9535015320294
MRC | Criteria | Characteristic |
---|---|---|
MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
HEAT | Heat Treatment | O-ANNEALED |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
ABGL | Width | 12.000 INCHES NOMINAL |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
ALBY | Usage Design | AIRCRAFT |
MRC | Decoded Requirement | Clear Text Reply |
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; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
MATT | Material | ALUMINUM ALLOY 2024 |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0320 INCHES NOMINAL |
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