799554CL5: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL ALLOY VANE, overall_width: 2.390 INCHES NOMINAL IN, overall_length: 8.740 INCHES NOMINAL IN, special_features: WAS VANE,TURBINE NOZZLE,TURBINE ENGINE, material_thickness: 1.245 INCHES NOMINAL IN, end_item_identification: TF-33 AIRCRAFT ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-962-1256, 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 | NICKEL ALLOY VANE |
| overall_width | 2.390 INCHES NOMINAL IN |
| overall_length | 8.740 INCHES NOMINAL IN |
| special_features | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE |
| material_thickness | 1.245 INCHES NOMINAL IN |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | FEAT |
| material_document_and_classification | AMS5388 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| NSN | 2840-00-962-1256 |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5388 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| OVERALL LENGTH | 8.740 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.390 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| MATERIAL THICKNESS | 1.245 INCHES NOMINAL IN |
| SPECIAL FEATURES | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY VANE |