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 Sheet Metal. component manufactured by Sae International, specifically under CAGE Code 0U583. It is also accompanied by the NSN 9535015317781 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 9535-01-531-7781, 9535015317781
MRC | Criteria | Characteristic |
---|---|---|
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
ALBY | USAGE DESIGN | AIRCRAFT |
CQHQ | MINIMUM YIELD STRENGTH | 39000 POUNDS PER SQUARE INCH |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
AARN | FABRICATION METHOD | ROLLED |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
CQBC | MINIMUM TENSILE STRENGTH | 59000 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 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 |