4063801: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include diameter: 23.672 INCHES NOMINAL IN, material: NICKEL ALLOY BLADE, overall_width: 1.840 INCHES NOMINAL IN, overall_length: 3.057 INCHES NOMINAL IN, special_features: THIS NSN IS AN F100 FRACTURE CRITICAL PART, blade_attachment_method: FIR TREE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-205-1280, 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 | 23.672 INCHES NOMINAL IN |
| material | NICKEL ALLOY BLADE |
| stage_number | 1 |
| overall_width | 1.840 INCHES NOMINAL IN |
| overall_length | 3.057 INCHES NOMINAL IN |
| special_features | THIS NSN IS AN F100 FRACTURE CRITICAL PART |
| blade_attachment_method | FIR TREE |
| end_item_identification | F15/F16 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | FEAT |
| material_document_and_classification | PWA1480 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-01-205-1280 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| SPECIAL FEATURES | THIS NSN IS AN F100 FRACTURE CRITICAL ITEM. T.O. 2J-F100-4, FIG 116, IND 47 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100 |
No substitute or cross-reference records for this part.