1864M32: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 4.117 INCHES NOMINAL IN, end_item_identification: ACFT ENG TF39, engine_section_location: HIGH PRESSURE TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-444-6553, 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 | NICKEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 2 |
| overall_length | 4.117 INCHES NOMINAL IN |
| end_item_identification | ACFT ENG TF39 |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-444-6553 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 4.117 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | DIFFERENT FROM 1864M32G02 NOTE LOCATION OF HOLES DRILLED ON STACKING AXIS OF AIRFOILS, ALSO NOTE THIS IS PART OF THE HT90 MOD FOR THE TF39 ENGINE, ALSO NOTE THE DRAWING NAME IS NOZZLE, HIGH PRESSURE TURBINE-STAGE 2 MACHINING, AND NOZZLE IS COATED WITH NICKEL PLATING, ALSO LENGTH IS 4.11745 |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |
| MATERIAL | NICKEL OVERALL |
No substitute or cross-reference records for this part.