Are you in need of part numbers AMS-QQ-A-250-4, AMS-QQ-A-250-4-CD351-0-250X48X12, AMS-QQ-A-250 4-T351-0.250X48X12, AMS-QQ-A-250-4-T351-0.250X48X12 from Society Of Automotive Engineers Inc, Sae International manufacturers of NSN 9535015317140? ASAP Parts Online has the part number in stock and ready to be shipped. Along with NSN 9535015317140 corresponding part numbers, we have access to billions of premium parts such as Plate Metal for the aviation, defense, and military industries. We are here to help streamline the process.
Alternative NSN: 9535-01-531-7140 |
Item Name:Plate Metal |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NIIN: 015317140 |
NCB Code: USA (01) |
Manufacturers: Sae International , Society Of Automotive Engineers Inc |
Part No Part No
|
Item Name Item Name
|
Manufacturer Manufacturer
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
AMS-QQ-A-250-4 | plate metal | Society Of Automotive Engineers Inc | Avl |
|
AMS-QQ-A-250-4 | plate metal | Sae International | Avl |
|
AMS-QQ-A-250-4-CD351-0-250X48X12 | plate metal | Society Of Automotive Engineers Inc | Avl |
|
AMS-QQ-A-250 4-T351-0.250X48X12 | plate metal | Society Of Automotive Engineers Inc | Avl |
|
AMS-QQ-A-250-4-T351-0.250X48X12 | plate metal | Sae International | Avl |
|
MRC | Criteria | Characteristic |
---|---|---|
CQBC | MINIMUM TENSILE STRENGTH | 64000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4 |
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.2500 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 64000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | T-351 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4 |
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 48.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.2500 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
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