482461: CASE,COMPRESSOR,AIRCRAFT GAS TUR.
CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 58.200 INCHES NOMINAL IN, material: STEEL CORROSION RESISTING OUTER CASE, design_type: AXIAL COMPRESSOR, special_features: HARDNESS RATE ROCKWELL C25-33 OR EQUIV., end_item_identification: TF-33 AIRCRAFT ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-966-3003, 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 | 58.200 INCHES NOMINAL IN |
| material | STEEL CORROSION RESISTING OUTER CASE |
| design_type | AXIAL COMPRESSOR |
| special_features | HARDNESS RATE ROCKWELL C25-33 OR EQUIV. |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| reference_data_and_literature | T.O. 2J-TF33-34 FIG 14, IND 1 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | CASE REAR COMPRESSOR |
| NSN | 2840-00-966-3003 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34 FIG 14, IND 1 |
| DIAMETER | 58.200 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | HARDNESS RATE ROCKWELL C25-33 OR EQUIV. |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CASE REAR COMPRESSOR |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| MATERIAL | STEEL CORROSION RESISTING OUTER CASE |
No substitute or cross-reference records for this part.