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-CDT351-1-0X6X24 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-CDT351-1-0X6X24 It is listed as Plate Metal. component manufactured by Society Of Automotiv, specifically under CAGE Code 81343. It is also accompanied by the NSN 9535015317800 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.
NSN Information for Part Number AMS-QQ-A-250-5-CDT351-1-0X6X24 with NSN 9535-01-531-7800, 9535015317800
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-531-7800 Item Description: PLATE,METAL | 9535 | 015317800 | N | |||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS-QQ-A-250/5-CDT351-1,0X6X24 | 5 | 9 | 5 |
Characteristics Data of NSN 9535-01-531-7800, 9535015317800
MRC | Criteria | Characteristic |
---|---|---|
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
CQHQ | MINIMUM YIELD STRENGTH | 42000 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 PLATE THICKNESS |
ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 24.000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |