Thank you for taking interest in Sae International part number AMS-T-7081-T6-0.312X0.049, which is listed with the NSN 4710-01-532-2361 and a product description of “Tube Metallic.” 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-T-7081-T6-0.312X0.049, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Tube Metallic part with the NSN 4710-01-532-2361. For example, you can browse other Sae International components that were produced under CAGE Code 0U583 or listings that belong to FSC 4710 Pipe Tube and Rigid Tubing 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-T-7081-T6-0.312X0.049 and other desired offerings on Aerospace Spare.
| 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-T6-0.312X0.049 | 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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