4084804: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include diameter: 14.497 INCHES MINIMUM AND 14.697 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, overall_width: 0.832 INCHES NOMINAL IN, overall_length: 6.809 INCHES NOMINAL IN, special_features: T.O. 2J-F100-14, FIG 130, IND 9; REPLACES P/N 4067004; TAKES 2 OF THIS ITEM TO MAKE UP BLADE SET P/N 4084194, blade_attachment_method: FIR TREE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-443-3613, 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 | 14.497 INCHES MINIMUM AND 14.697 INCHES MAXIMUM IN |
| design_type | AXIAL COMPRESSOR |
| stage_number | 4 |
| overall_width | 0.832 INCHES NOMINAL IN |
| overall_length | 6.809 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-14, FIG 130, IND 9; REPLACES P/N 4067004; TAKES 2 OF THIS ITEM TO MAKE UP BLADE SET P/N 4084194 |
| blade_attachment_method | FIR TREE |
| end_item_identification | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | ABHP AND CZBJ AND ABMZ AND ABMK AND FEAT |
| NSN | 2840-01-443-3613 |
| STAGE NUMBER | 4 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND CZBJ AND ABMZ AND ABMK AND FEAT |
| BLADE ATTACHMENT METHOD | FIR TREE |
| DIAMETER | 14.497 INCHES MINIMUM AND 14.697 INCHES MAXIMUM IN |
| OVERALL LENGTH | 6.809 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.832 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 130, IND 9; REPLACES P/N 4067004; TAKES 2 OF THIS ITEM TO MAKE UP BLADE SET P/N 4084194 |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.