SHROUD,COMPRESSOR,AIRCRAFT GAS T. Key specifications include diameter: 24.000 INCHES NOMINAL IN, material: STEEL CORROSION RESISTING OVERALL, overall_length: 7.000 INCHES NOMINAL IN, end_item_identification: TF33 AIRCRAFT ENGINE, engine_section_location: DIFFUSER, reference_data_and_literature: T.O. 2J-TF33-4 FIG 23 IND 57.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-966-2986, 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 | 24.000 INCHES NOMINAL IN |
| material | STEEL CORROSION RESISTING OVERALL |
| overall_length | 7.000 INCHES NOMINAL IN |
| end_item_identification | TF33 AIRCRAFT ENGINE |
| engine_section_location | DIFFUSER |
| reference_data_and_literature | T.O. 2J-TF33-4 FIG 23 IND 57 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | SHROUD ASSEMBLY HIGH PRESSURE COMPRESSOR |
| NSN | 2840-00-966-2986 |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| DIAMETER | 24.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | DIFFUSER |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 23 IND 57 |
| MATERIAL | STEEL CORROSION RESISTING OVERALL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHROUD ASSEMBLY HIGH PRESSURE COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 7.000 INCHES NOMINAL IN |