VANE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 30.400 INCHES MINIMUM AND 30.430 INCHES MAXIMUM IN, material: STEEL CORROSION RESISTING OVERALL, overall_length: 1.809 INCHES MINIMUM AND 1.811 INCHES MAXIMUM IN, precious_material: SILVER, end_item_identification: TF-33 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-981-1804, 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 | 30.400 INCHES MINIMUM AND 30.430 INCHES MAXIMUM IN |
| material | STEEL CORROSION RESISTING OVERALL |
| overall_length | 1.809 INCHES MINIMUM AND 1.811 INCHES MAXIMUM IN |
| precious_material | SILVER |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O.2J-TF33-4 FIG14, IND11 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | COMPRESSOR STATOR HALF 5 STAGE, ASSY OF |
| NSN | 2840-00-981-1804 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 30.400 INCHES MINIMUM AND 30.430 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| PRECIOUS MATERIAL | SILVER |
| REFERENCE DATA AND LITERATURE | T.O.2J-TF33-4 FIG14, IND11 |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL | STEEL CORROSION RESISTING OVERALL |
| OVERALL LENGTH | 1.809 INCHES MINIMUM AND 1.811 INCHES MAXIMUM IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPRESSOR STATOR HALF 5 STAGE, ASSY OF |