599452: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: ALUMINUM ALLOY OVERALL, overall_length: 1.496 INCHES MINIMUM AND 1.504 INCHES MAXIMUM IN, end_item_identification: TF33 AIRCRAFT ENGINE, engine_section_location: TURBINE, reference_data_and_literature: T.O. 2J-TF33-4 FIG32 IND2, criticality_code_justification: AGAV.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-419-2013, 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 | ALUMINUM ALLOY OVERALL |
| stage_number | 2 |
| overall_length | 1.496 INCHES MINIMUM AND 1.504 INCHES MAXIMUM IN |
| end_item_identification | TF33 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| reference_data_and_literature | T.O. 2J-TF33-4 FIG32 IND2 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | SHROUD TURBINE STATOR,2 STAGE, ASSY OF |
| NSN | 2840-01-419-2013 |
| STAGE NUMBER | 2 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG32 IND2 |
| OVERALL LENGTH | 1.496 INCHES MINIMUM AND 1.504 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHROUD TURBINE STATOR,2 STAGE, ASSY OF |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| MATERIAL | ALUMINUM ALLOY OVERALL |
No substitute or cross-reference records for this part.