GANG CHANNEL,BOLT,TURBINE ENGINE. Key specifications include material: STEEL COMP 302 OVERALL, end_style: SPRING END,SQUARED AND GROUND BOTH ENDS, load_rating: 6.039 POUNDS NOMINAL LBS, bore_diameter: 0.500 INCHES NOMINAL IN, stock_diameter: 0.038 INCHES NOMINAL IN, inside_diameter: 0.396 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 2840-00-859-3323, 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 COMP 302 OVERALL |
| end_style | SPRING END,SQUARED AND GROUND BOTH ENDS |
| load_rating | 6.039 POUNDS NOMINAL LBS |
| bore_diameter | 0.500 INCHES NOMINAL IN |
| stock_diameter | 0.038 INCHES NOMINAL IN |
| inside_diameter | 0.396 INCHES NOMINAL IN |
| style_designator | CYLINDRICAL |
| surface_treatment | PASSIVATE OVERALL |
| spring_free_length | 1.250 INCHES NOMINAL IN |
| spring_solid_length | 0.327 INCHES NOMINAL IN |
| coil_helix_direction | LEFT-HAND |
| spring_deflection_rate | 8.330 POUNDS PER INCH NOMINAL LBS |
| NSN | 2840-00-859-3323 |
| END ITEM IDENTIFICATION | J57 AIRCRAFT ENGINE |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | T.O. 2J-J57-54; BOLT-NOZZLE ASSY;STAGES 1-3; 1 UNIT PER ASSY; COMBUSTION CHAMBER |