The parts under NSN 9535-01-531-7783 of Sheet Metal manufactured by Society Of Automotive Engineers Inc, Sae International is available in our inventory. An ASAP Semiconductor Website, ASAP Aviation Stock has access to over three billion parts, paired with easy-to-use search engines that enable our customers to browse through our inventory quickly and efficiently. Our focus on quality control has earned us our AS9120B, ISO 9001:2015, and FAA 0056B certification, and we are the only independent distributor with a No China Sourcing pledge. If you are ready to get started, you can send us a Request for Quote for the parts with 9535-01-531-7783 from this webpage, and one of our account managers will give you a quote for parts like AMS QQ A 250 5 T3 0 016X12X36, AMS-QQ-A-250 5-CDT3-0 016X12X36, AMS-QQ-A-250 5, AMS-QQ-A-250 5-T3-0.016X12X36 within fifteen minutes.
Alternative NSN: 9535-01-531-7783 |
Item Name:Sheet Metal |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NIIN: 015317783 |
NCB Code: USA (01) |
Manufacturers: Sae International , Society Of Automotive Engineers Inc |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
AMS QQ A 250 5 T3 0 016X12X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5-CDT3-0 016X12X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5-T3-0.016X12X36 | sae international | sheet metal | Avl | RFQ |
AMS-QQ-A-250 5 | sae international | sheet metal | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0160 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 | 59000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 39000 POUNDS PER SQUARE INCH |
FEAT | SPECIAL FEATURES | THIN LAYERS APPROXIMATELY EQUAL THICKNESS OF ALUMINUM ALLOY 1230 ANODIC TO 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 |
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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