CHAMBER,COMBUSTION,ENGINE STARTE. Key specifications include material: STEEL OVERALL, hole_diameter: 0.311 INCHES NOMINAL IN, outside_diameter: 0.591 INCHES NOMINAL IN, style_designator: SPLIT HELICAL-RIGHT HAND, surface_treatment: ZINC OVERALL, material_thickness: 0.078 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 2995-00-866-8071, 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 OVERALL |
| hole_diameter | 0.311 INCHES NOMINAL IN |
| outside_diameter | 0.591 INCHES NOMINAL IN |
| style_designator | SPLIT HELICAL-RIGHT HAND |
| surface_treatment | ZINC OVERALL |
| material_thickness | 0.078 INCHES NOMINAL IN |
| end_item_identification | 2320-01-452-5579 |
| NSN | 2995-00-866-8071 |
| OVERALL HEIGHT | 4.470 INCHES MINIMUM AND 4.600 INCHES MAXIMUM IN |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | THERE ARE 3 ATTACHED TUBE ASSEMBLYS;INSIDE DIA. 7.244 MIN.& 7.250 MAX. |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CHAMBER ASSEMBLY ENGINE STARTER |
| OVERALL DIAMETER | 8.990 INCHES MINIMUM AND 9.010 INCHES MAXIMUM IN |
| REFERENCE DATA AND LITERATURE | T.O. 2JA3-38-4 |
| END ITEM IDENTIFICATION | STARTER,ENGINE,GAS TURBINE P/N 383242-1-8,USAF TYPE STU-20/A34;U/O J79-15 |