| Part Number: AMS T 7081 T6 0 312X0 025 | Manufacturer: Society Of Automotive Engineers Inc |
| NSN : 4710-01-532-2363 (4710015322363) | Item Name : tube metallic |
| CAGE Code: 81343 | FSC : 4710 Pipe Tube and Rigid Tubing |
| Alternate P/N : AMST7081T60312X0025 | INC Code: 31979 |
| NIIN : 01-532-2363 (015322363) | FSG : 47 Pipe Tubing Hose and Fittings |
| Country: USA | NCB Code: 01 |
Would you like to obtain a quick quote for Society Of Automotive Engineers Inc(Cage Code 81343) Part Number AMS T 7081 T6 0 312X0 025Tube Metallicwith NSN 4710015322363? it's just a few steps away! Simply complete the form in its entirety, and we will promptly reply with a quote within 15 minutes. This is an excellent opportunity to get the quick quote for AMS T 7081 T6 0 312X0 025, so take advantage of it right away.
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| MRC | Criteria | Characteristic |
|---|---|---|
| AAGR | CROSS-SECTIONAL SHAPE STYLE | PLAIN ROUND |
| AAGT | WALL THICKNESS | 0.025 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 | 0.025 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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