Using the Request for Quote (RFQ) form provided on this page, you can request competitive procurement options on part number AMS-QQ-A-250 5 with rapid responses always offered by our staff. To ensure that you locate and procure exactly what you need with ease, we list parts with as much information as we can. For example, part number AMS-QQ-A-250 5 It is listed as Plate Metal. component manufactured by Sae International, specifically under CAGE Code 0U583. It is also accompanied by the NSN 9535015317803 for ease of organization, the first digits of the NSN indicating that the part belongs to FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal.
Characteristics Data of NSN 9535-01-531-7803, 9535015317803
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
CQBC | MINIMUM TENSILE STRENGTH | 62000 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 PLATE THICKNESS |
AGTA | BASIC SHAPE STYLE | SOLID |
AARN | FABRICATION METHOD | ROLLED |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.2500 INCHES NOMINAL |
ALBY | USAGE DESIGN | AIRCRAFT |
CQHQ | MINIMUM YIELD STRENGTH | 40000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |