Thank you for taking interest in Society Of Automotive Engineers Inc part number AMS QQ A 250 5 T3 0 071X12X48, which is listed with the NSN 9535-01-531-7798 and a product description of “Sheet Metal.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number AMS QQ A 250 5 T3 0 071X12X48, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Sheet Metal part with the NSN 9535-01-531-7798. For example, you can browse other Society Of Automotive Engineers Inc components that were produced under CAGE Code 81343 or listings that belong to FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number AMS QQ A 250 5 T3 0 071X12X48 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-7798 Item PartTypeName: SHEET,METAL | 9535 | 015317798 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/5-T3-0.071X12X48 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 40000 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 40000 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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