1881M89G03: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include design_type: AXIAL COMPRESSOR, overall_height: 3.351 INCHES NOMINAL IN, overall_length: 1.883 INCHES MINIMUM AND 1.888 INCHES MAXIMUM IN, end_item_identification: TF-39 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: HIGH PRESSURE TURBINE, criticality_code_justification: ABHP AND ABKW AND FEAT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-444-7000, 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.
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_height | 3.351 INCHES NOMINAL IN |
| overall_length | 1.883 INCHES MINIMUM AND 1.888 INCHES MAXIMUM IN |
| end_item_identification | TF-39 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | ABHP AND ABKW AND FEAT |
| NSN | 2840-01-444-7000 |
| OVERALL HEIGHT | 3.351 INCHES NOMINAL IN |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABKW AND FEAT |
| OVERALL LENGTH | 1.883 INCHES MINIMUM AND 1.888 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | T.O. 2J-TF39-4, FIG 61, IND 1; ECP 369, DCN 97-37; 1.451 IN. BETWEEN NOZZLE AIR FLOW CAVITIES OC; 1.703 LENGTH OF NOZZLE FIN; 1.415 WIDTH OF NOZZLE FIN; REDUCED AREA, CONTROLLED; REPL P/N 9082M95G17; NOT TO BE GRPED PER ECP/DCN; WHOLE NEW CONFIGURATION; AS THE OLD CONFIG IS REPLACED BY TCTO KITS WITH THIS NEW ITEM, THE OLD CONFIG IS THROWN AWAY IN |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.