4080332: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 3.842 INCHES NOMINAL IN, special_features: THIS NSN IS AN F100 FRACTURE CRITICAL PART. T.O.
2J-F100-14, FIG 121, IND 44, fsc_application_data: F-15 AIRCRAFT, blade_attachment_method: FIR TREE, end_item_identification: F100-PW-200/220 ACFT ENGINES. This part is cataloged in the U.S. Government catalog under NSN 2840-01-366-3768, 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.
| design_type | AXIAL COMPRESSOR |
| stage_number | 2 |
| overall_length | 3.842 INCHES NOMINAL IN |
| special_features | THIS NSN IS AN F100 FRACTURE CRITICAL PART. T.O. 2J-F100-14, FIG 121, IND 44 |
| fsc_application_data | F-15 AIRCRAFT |
| blade_attachment_method | FIR TREE |
| end_item_identification | F100-PW-200/220 ACFT ENGINES |
| engine_section_location | TURBINE |
| criticality_code_justification | FEAT |
| NSN | 2840-01-366-3768 |
| FSC APPLICATION DATA | F-15 AIRCRAFT |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 3.842 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | THIS NSN IS AN F100 FRACTURE CRITICAL PART. T.O. 2J-F100-14, FIG 121, IND 44 |
| END ITEM IDENTIFICATION | F100-PW-200/220 ACFT ENGINES |
No substitute or cross-reference records for this part.