9395M67P01: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include diameter: 28.450 INCHES MINIMUM AND 28.465 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-TF39-4, FIG 67 IND 38; MADE ALTERNATE JAN 94 FOR MAINTENANCE ECONOMY PER T.O.
2J-TF39-4S-2, end_item_identification: ACFT ENG TF39, engine_section_location: LOW PRESSURE TURBINE. This part is cataloged in the U.S. Government catalog under NSN 2840-01-163-6701, 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.
| diameter | 28.450 INCHES MINIMUM AND 28.465 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 5 |
| special_features | T.O. 2J-TF39-4, FIG 67 IND 38; MADE ALTERNATE JAN 94 FOR MAINTENANCE ECONOMY PER T.O. 2J-TF39-4S-2 |
| end_item_identification | ACFT ENG TF39 |
| engine_section_location | LOW PRESSURE TURBINE |
| criticality_code_justification | FEAT AND CZCJ AND CZBJ |
| NSN | 2840-01-163-6701 |
| STAGE NUMBER | 5 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT AND CZCJ AND CZBJ |
| DIAMETER | 28.450 INCHES MINIMUM AND 28.465 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | T.O. 2J-TF39-4, FIG 67 IND 38; MADE ALTERNATE JAN 94 FOR MAINTENANCE ECONOMY PER T.O. 2J-TF39-4S-2 |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.