Thank you for taking an interest in our selection of 4710-01-532-2367 parts here on Boost AOG. You are currently on the RFQ form for part number AMS-T-7081-T6-0.250X0.035, a Society Of Automotive Engineers Inc product listed with the Tube Metallic If part number AMS-T-7081-T6-0.250X0.035 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.
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To ensure the quality of our NSN components, we adhere to a strict NO CHINA SOURCING pledge, meaning every purchased item will be delivered alongside any pertinent qualifying certifications or manufacturing trace documentation for your benefit. Paired with numerous other commitments, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. If you happen to be facing a time constraint and require NSN parts quickly, contact us at your earliest convenience, and we will discuss the expedited shipping options we have available for domestic and international customers alike. With our various dedications in mind, kick off procurement for Society Of Automotive Engineers Inc part number AMS-T-7081-T6-0.250X0.035 and other Tube Metallic products today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 4710-01-532-2367 Item PartTypeName: TUBE,METALLIC | 4710 | 015322367 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-T-7081-T6-0.250X0.035 | 1 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAGR | CROSS-SECTIONAL SHAPE STYLE | PLAIN ROUND |
| AAGT | WALL THICKNESS | 0.035 INCHES NOMINAL |
| AAGZ | FIRST END STYLE | PLAIN |
| ABMZ | DIAMETER | 0.250 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 | 0.035 INCHES NOMINAL |
| AAGZ | FIRST END STYLE | PLAIN |
| ABMZ | DIAMETER | 0.250 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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