748681: VANE,COMPRESSOR,AIRCRAFT GAS TUR.
VANE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: STEEL CORROSION RESISTING OVERALL, stage_number: 11, overall_length: 2.482 INCHES MINIMUM AND 2.494 INCHES MAXIMUM IN, special_features: CONSISTS OF 122 VANES; INNER AND OUTER SHROUDS; AIR SEALING RING, end_item_identification: TF33 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-004-1799, 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 | STEEL CORROSION RESISTING OVERALL |
| stage_number | 11 |
| overall_length | 2.482 INCHES MINIMUM AND 2.494 INCHES MAXIMUM IN |
| special_features | CONSISTS OF 122 VANES; INNER AND OUTER SHROUDS; AIR SEALING RING |
| end_item_identification | TF33 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-TF33-4, FIG17, IND11 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | COMPRESSOR STATOR 11 STAGE,ASSY OF |
| NSN | 2840-01-004-1799 |
| STAGE NUMBER | 11 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG17, IND11 |
| OVERALL LENGTH | 2.482 INCHES MINIMUM AND 2.494 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | CONSISTS OF 122 VANES; INNER AND OUTER SHROUDS; AIR SEALING RING |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPRESSOR STATOR 11 STAGE,ASSY OF |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| MATERIAL | STEEL CORROSION RESISTING OVERALL |
No substitute or cross-reference records for this part.