2666969: SHAFT,SHOULDERED.
The SHAFT,SHOULDERED is a the manufacturer industrial component. Key specifications include material: STEEL CORROSION RESISTING, end_similarity: NOT IDENTICAL, overall_length: 2.620 INCHES NOMINAL IN, surface_finish: 125.0 MICROINCHES, first_end_style: EXTERNAL THREADED, second_end_style: CIRCULAR GROOVED, CROSS DRILLED HOLE, AND EXTERNALLY THREADED. This part is cataloged in the U.S.
Government catalog under NSN 3040-01-122-7747, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | STEEL CORROSION RESISTING |
| step_quantity | 2 |
| end_similarity | NOT IDENTICAL |
| overall_length | 2.620 INCHES NOMINAL IN |
| surface_finish | 125.0 MICROINCHES |
| first_end_style | EXTERNAL THREADED |
| second_end_style | CIRCULAR GROOVED, CROSS DRILLED HOLE, AND EXTERNALLY THREADED |
| special_features | THREAD DATA 1ST END 0.190-56UNS-3A,2ND END 0.125-40UNC-3A,1ST END INTERNAL CENTER HOLE 0.160 IN. MIN AND 0.220 IN MAX DP A |
| first_end_diameter | 0.1900 INCHES NOMINAL IN |
| second_end_diameter | 0.1250 INCHES NOMINAL IN |
| fsc_application_data | AIRCRAFT ENGINE FUEL SYSTEM |
| largest_step_diameter | 0.190 INCHES NOMINAL IN |
| NSN | 3040-01-122-7747 |
| SURFACE FINISH | 125.0 MICROINCHES |
| FSC APPLICATION DATA | AIRCRAFT ENGINE FUEL SYSTEM |
| SECOND END HOLE DIAMETER | 0.0312 INCHES NOMINAL IN |
| SECOND END EXTERNAL THREAD LENGTH | 0.340 INCHES NOMINAL IN |
| STEP QUANTITY | 2 |
| FIRST END DIAMETER | 0.1900 INCHES NOMINAL IN |
| SECOND END DIAMETER | 0.1250 INCHES NOMINAL IN |
| LARGEST STEP DIAMETER | 0.190 INCHES NOMINAL IN |
| FIRST END EXTERNAL THREAD LENGTH | 0.410 INCHES NOMINAL IN |
| FIRST END STYLE | EXTERNAL THREADED |