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-T81-0.040X12X36 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-T81-0.040X12X36 It is listed as Sheet Metal. component manufactured by Sae International, specifically under CAGE Code 0U583. It is also accompanied by the NSN 9535015317795 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 9535-01-531-7795, 9535015317795
MRC | Criteria | Characteristic |
---|---|---|
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AARN | FABRICATION METHOD | ROLLED |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ALBY | USAGE DESIGN | AIRCRAFT |
CQHQ | MINIMUM YIELD STRENGTH | 54000 POUNDS PER SQUARE INCH |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | SOLID |
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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |