4080704: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: STEEL BLADE, design_type: AXIAL COMPRESSOR, overall_length: 6.848 INCHES NOMINAL IN, special_features: T.O. 2J-F100-54; 66 UNITS PER ASSY, blade_attachment_method: SLOT, end_item_identification: F100PW0229 ACFT ENGINE/FDT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-372-4900, 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 | STEEL BLADE |
| design_type | AXIAL COMPRESSOR |
| stage_number | 4 |
| overall_length | 6.848 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-54; 66 UNITS PER ASSY |
| blade_attachment_method | SLOT |
| end_item_identification | F100PW0229 ACFT ENGINE/FDT |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | ABHP AND APGF AND CZBJ AND CZCJ |
| NSN | 2840-01-372-4900 |
| STAGE NUMBER | 4 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND APGF AND CZBJ AND CZCJ |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 6.848 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-54; 66 UNITS PER ASSY |
| END ITEM IDENTIFICATION | F100PW0229 ACFT ENGINE/FDT |
| MATERIAL | STEEL BLADE |
No substitute or cross-reference records for this part.