4082504: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 6.929 INCHES NOMINAL IN, special_features: NOT TO BE PROCURED; NSN REQUIRED; THIS IS A SINGLE ROBUST BLADE, blade_attachment_method: FIR TREE, end_item_identification: F100PW229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-425-7589, 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 | 4 |
| overall_length | 6.929 INCHES NOMINAL IN |
| special_features | NOT TO BE PROCURED; NSN REQUIRED; THIS IS A SINGLE ROBUST BLADE |
| blade_attachment_method | FIR TREE |
| end_item_identification | F100PW229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | APGF AND CZBJ AND CZCJ AND BGLW AND ABHP |
| NSN | 2840-01-425-7589 |
| STAGE NUMBER | 4 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND ABHP |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 6.929 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | NOT TO BE PROCURED; NSN REQUIRED; THIS IS A SINGLE ROBUST BLADE |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.