Part Number : AMS-QQ-A-250 4-T81-0.100X48X12
Alternate P/N: AMSQQA2504T810100X48X12
NSN : 9535-01-531-7138
Item Name : Sheet Metal
Manufacturer : Society Of Automotive Engineers Inc
CAGE Code : 81343
Qty Available : 1528
Last Updated : 05-12-2024
Thank you for choosing ASAP Semiconductor’s website ASAP 360 Unlimited for your NSN part requirement. We have NSN part number AMS-QQ-A-250 4-T81-0.100X48X12 in stock. This NATO part is manufactured by Society Of Automotive Engineers Inc. It is listed as Sheet Metal. The national stock number that is associated with NSN part AMS-QQ-A-250 4-T81-0.100X48X12 is 9535015317138. All the NSN parts we delivered such as AMS-QQ-A-250 4-T81-0.100X48X12 are passed through quality checks.
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ASAP Semiconductor prides itself for providing the right technology at the right place just in time and at an aggressive price. Feel free to browse ASAP360Unlimited.com for other parts made by Society Of Automotive Engineers Inc or parts that belong to the same federal supply 9535 Plate Sheet Strip and Foil Nonferrous Base Metal or federal supply group 95 Metal Bars Sheets and Shapes With over 20 million parts ready for immediate delivery around the globe, we will strive to be your first choice for purchasing.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-531-7138 Item Description: Sheet Metal | 9535 | 015317138 | N | A | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
A | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
Ams-Qq-A-250-4 | 5 | 1 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED" |
ABGL | WIDTH | 12.000 INCHES NOMINAL" |
ABRY | LENGTH | 48.000 INCHES NOMINAL" |
ADVM | CROSS-SECTIONAL THICKNESS | 0.1000 INCHES NOMINAL" |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT" |
AGTA | BASIC SHAPE STYLE | SOLID" |
ALBY | USAGE DESIGN | AIRCRAFT" |
CQBC | MINIMUM TENSILE STRENGTH | 67000 POUNDS PER SQUARE INCH" |
CQHQ | MINIMUM YIELD STRENGTH | 58000 POUNDS PER SQUARE INCH" |
HEAT | HEAT TREATMENT | T-81 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 | 0.1000 INCHES NOMINAL" |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT" |
AGTA | BASIC SHAPE STYLE | SOLID" |
ALBY | USAGE DESIGN | AIRCRAFT" |
CQBC | MINIMUM TENSILE STRENGTH | 67000 POUNDS PER SQUARE INCH" |
CQHQ | MINIMUM YIELD STRENGTH | 58000 POUNDS PER SQUARE INCH" |
HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED" |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4" |
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