The SEMICONDUCTOR DEVICE,DIODE is a the manufacturer industrial component. Key specifications include material: GLASS ENCLOSURE, bore_type: SERRATED, head_style: HEXAGON, head_height: 0.281 INCHES NOMINAL IN, thread_class: 1A A, overall_width: 1.000 INCHES NOMINAL IN. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1680-00-571-0667, 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 | GLASS ENCLOSURE |
| bore_type | SERRATED |
| head_style | HEXAGON |
| head_height | 0.281 INCHES NOMINAL IN |
| thread_class | 1A A |
| overall_width | 1.000 INCHES NOMINAL IN |
| thread_length | 0.562 INCHES MINIMUM IN |
| major_diameter | 0.750 INCHES NOMINAL IN |
| minor_diameter | 0.562 INCHES NOMINAL IN |
| overall_length | 0.230 INCHES MINIMUM AND 0.300 INCHES MAXIMUM IN |
| shoulder_shape | ROUND FIRST SHOULDER |
| fastener_length | 1.772 INCHES NOMINAL IN |
| NSN | 1680-00-571-0667 |
| OVERALL WIDTH | 1.000 INCHES NOMINAL IN |
| MATERIAL | ALUMINUM ALLOY |
| SERRATION QUANTITY | 24 |
| LINK END THICKNESS | 0.190 INCHES NOMINAL IN |
| FEATURES PROVIDED | COUNTERBORE |
| LINK END HOLE DIAMETER | 0.620 INCHES NOMINAL IN |
| SHAFT END THICKNESS | 0.416 INCHES NOMINAL IN |
| CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.380 INCHES NOMINAL IN |
| END ITEM IDENTIFICATION | TURBINE ENGINE FUEL CONTROL, AIRCRAFT |
| MINOR DIAMETER | 0.562 INCHES NOMINAL IN |