At NSN Unlimited, we maintain a large database of parts AMS QQ A 250 5 T3 0 125X6X36, AMS-QQ-A-250 5, AMS-QQ-A-250 5-CDT3-0 125X6X36, AMS-QQ-A-250 5-T3-0.125X6X36, AMS-QQ-A-250-5 with NSN 9535-01-531-7799 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Society Of Automotive Engineers Inc, Sae International. Utilize our interface to browse items by part number, part type, manufacturer, and more. Obtain insights on top MRO and FBO services, Manufacturer profiles, and part catalogs.
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Alternative NSN: 9535-01-531-7799 |
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: 015317799 |
NCB Code: USA (01) |
Manufacturers: Society Of Automotive Engineers Inc , Sae International |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
AMS QQ A 250 5 T3 0 125X6X36 | 9535-01-531-7799 | sheet metal | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-250 5 | 9535-01-531-7799 | sheet metal | sae international | Avl | RFQ |
AMS-QQ-A-250 5-CDT3-0 125X6X36 | 9535-01-531-7799 | sheet metal | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-250 5-T3-0.125X6X36 | 9535-01-531-7799 | sheet metal | sae international | Avl | RFQ |
AMS-QQ-A-250-5 | 9535-01-531-7799 | sheet metal | society of automotive engineers inc | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
ALBY | III USAGE DESIGN | AIRCRAFT |
ADVM | CROSS-SECTIONAL THICKNESS | 0.1250 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 40000 POUNDS PER SQUARE INCH |
AARN | FABRICATION METHOD | ROLLED |
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 |
AGTA | BASIC SHAPE STYLE | SOLID |
HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
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