389679: CASE,COMPRESSOR,AIRCRAFT GAS TUR.
CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include design_type: COMPRESSOR, overall_width: 22.025 INCHES MINIMUM AND 22.113 INCHES MAXIMUM IN, special_features: ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE, end_item_identification: TF-33 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR, reference_data_and_literature: 2J-TF33-4. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-765-9953, 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 | COMPRESSOR |
| overall_width | 22.025 INCHES MINIMUM AND 22.113 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | 2J-TF33-4 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | CASE REAR COMPRESSOR, ASSY OF |
| NSN | 2840-00-765-9953 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-TF33-4 |
| OVERALL WIDTH | 22.025 INCHES MINIMUM AND 22.113 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CASE REAR COMPRESSOR, ASSY OF |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.