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-CDT3-0 032X6X36 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-CDT3-0 032X6X36 It is listed as Sheet Metal. component manufactured by Society Of Automotive Engineers Inc, specifically under CAGE Code 81343. It is also accompanied by the NSN 9535015317790 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-CDT3-0 032X6X36 with NSN 9535-01-531-7790, 9535015317790
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-531-7790 Item Description: SHEET,METAL | 9535 | 015317790 | N | |||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS-QQ-A-250/5-CDT3-0,032X6X36 | 5 | 9 | 5 |
Characteristics Data of NSN 9535-01-531-7790, 9535015317790
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 |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
CQHQ | MINIMUM YIELD STRENGTH | 39000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
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 |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |