111R643G03: NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.
NOZZLE ASSEMBLY,TURBINE,AIRCRAFT. Key specifications include material: CHROMIUM ALLOY OVERALL, overall_width: 12.000 INCHES NOMINAL IN, overall_height: 12.000 INCHES NOMINAL IN, overall_length: 24.000 INCHES NOMINAL IN, special_features: THIS TURBINE NOZZLE ASSY HAS A CRITICAL TOLERANCE,FIT RESTRICTION,AND APPLICATION, end_item_identification: ACFT ENG J79, J85, T58, T64. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-944-3276, 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 | CHROMIUM ALLOY OVERALL |
| overall_width | 12.000 INCHES NOMINAL IN |
| overall_height | 12.000 INCHES NOMINAL IN |
| overall_length | 24.000 INCHES NOMINAL IN |
| special_features | THIS TURBINE NOZZLE ASSY HAS A CRITICAL TOLERANCE,FIT RESTRICTION,AND APPLICATION |
| end_item_identification | ACFT ENG J79, J85, T58, T64 |
| engine_section_location | TURBINE |
| reference_data_and_literature | 2J-J79-64 FIG 28 IND1 |
| criticality_code_justification | FEAT |
| NSN | 2840-00-944-3276 |
| OVERALL HEIGHT | 12.000 INCHES NOMINAL IN |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| REFERENCE DATA AND LITERATURE | 2J-J79-64 FIG 28 IND1 |
| OVERALL LENGTH | 24.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 12.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | THIS TURBINE NOZZLE ASSY HAS A CRITICAL TOLERANCE,FIT RESTRICTION,AND APPLICATION |
| END ITEM IDENTIFICATION | ACFT ENG J79, J85, T58, T64 |
| MATERIAL | CHROMIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.