Thank you for considering Society Of Automotive Engineers Inc part number AMS-T-7081-T6-0.312X0.049, a component we stock that is further identified by the NSN 4710-01-532-2361 and product description “Tube Metallic.” This item is currently available for purchase on our website today, and you can obtain a tailored quote at any time by completing the form on this page. To help us provide the best solution, please include critical details like your quantity requirements, target pricing, and delivery preferences within the submitted request. Once we receive your form, our team will promptly review provided information and respond with a quote that aligns with your needs.
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Alongside part number AMS-T-7081-T6-0.312X0.049, we encourage you to explore other offerings we carry from Society Of Automotive Engineers Inc that have been produced under CAGE Code 81343, as well as similar products classified under FSC 4710 Pipe Tube and Rigid Tubing that may suit your projects. We can help you obtain pricing on all items that you are interested in, securing the most optimal solution for you. We are also happy to discuss any requirements that you may have, presenting specialized options for many restrictions and needs alike. With our services in mind, please submit your request for part number AMS-T-7081-T6-0.312X0.049 today and discover why Marine Defence Parts is a trusted partner for naval and defense procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 4710-01-532-2361 Item PartTypeName: TUBE,METALLIC | 4710 | 015322361 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-T-7081 | 1 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAGR | CROSS-SECTIONAL SHAPE STYLE | PLAIN ROUND |
| AAGT | WALL THICKNESS | 0.049 INCHES NOMINAL |
| AAGZ | FIRST END STYLE | PLAIN |
| ABMZ | DIAMETER | 0.312 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| CQBB | SECOND END RELATIONSHIP WITH FIRST END | IDENTICAL |
| CQCF | CONSTRUCTION | SEAMLESS |
| FEAT | SPECIAL FEATURES | PSUPPLIED IN MILL LENGTHS; ULTIMATE TENSILE STRENGTH 42000.0 POUNDS PER SQUARE INCH (PSI) MINIMUM; YIELD STRENGTH 35000.0 PSI MINIMUM; USED IN HYDRAULIC AND PNEUMATIC SYSTEMS OF AIRCRAFT, INCLUDING 3000.0 PSI SYSTEMS |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED AND ARTIFICIALLY AGED |
| MATT | MATERIAL | ALUMINUM ALLOY 6061 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-T-7081 ASSN STD SINGLE MATERIAL RESPONSE |
| AAGR | CROSS-SECTIONAL SHAPE STYLE | PLAIN ROUND |
| AAGT | WALL THICKNESS | 0.049 INCHES NOMINAL |
| AAGZ | FIRST END STYLE | PLAIN |
| ABMZ | DIAMETER | 0.312 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| CQBB | SECOND END RELATIONSHIP WITH FIRST END | IDENTICAL |
| CQCF | CONSTRUCTION | SEAMLESS |
| FEAT | SPECIAL FEATURES | PSUPPLIED IN MILL LENGTHS; ULTIMATE TENSILE STRENGTH 42000.0 POUNDS PER SQUARE INCH (PSI) MINIMUM; YIELD STRENGTH 35000.0 PSI MINIMUM; USED IN HYDRAULIC AND PNEUMATIC SYSTEMS OF AIRCRAFT, INCLUDING 3000.0 PSI SYSTEMS |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED AND ARTIFICIALLY AGED |
| MATT | MATERIAL | ALUMINUM ALLOY 6061 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-T-7081 ASSN STD SINGLE MATERIAL RESPONSE |
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