495254CL9: 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: ORIGINAL NAME VANE,TURBINE NOZZLE,TURBINE ENGINE, material_thickness: 1.245 INCHES NOMINAL IN, end_item_identification: ACFT ENG TF-33. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-962-1266, 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 | ORIGINAL NAME VANE,TURBINE NOZZLE,TURBINE ENGINE |
| material_thickness | 1.245 INCHES NOMINAL IN |
| end_item_identification | ACFT ENG TF-33 |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS 5388 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| NSN | 2840-00-962-1266 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5388 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 | ORIGINAL NAME VANE,TURBINE NOZZLE,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG TF-33 |
| MATERIAL | NICKEL ALLOY VANE |