4084503: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_height: 5.077 INCHES MINIMUM AND 5.089 INCHES MAXIMUM IN, overall_length: 0.796 INCHES NOMINAL IN, special_features: SURFACE TREATMENT PWA 694 COBALT ALLOY; IT TAKES OF THESE TO MAKE UP BLADE SET P/N 4084283, blade_attachment_method: FIR TREE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-443-4087, 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 | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| overall_height | 5.077 INCHES MINIMUM AND 5.089 INCHES MAXIMUM IN |
| overall_length | 0.796 INCHES NOMINAL IN |
| special_features | SURFACE TREATMENT PWA 694 COBALT ALLOY; IT TAKES OF THESE TO MAKE UP BLADE SET P/N 4084283 |
| blade_attachment_method | FIR TREE |
| end_item_identification | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | CZBJ AND CZCJ AND ABHP AND ABKW AND FEAT |
| NSN | 2840-01-443-4087 |
| OVERALL HEIGHT | 5.077 INCHES MINIMUM AND 5.089 INCHES MAXIMUM IN |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND CZCJ AND ABHP AND ABKW AND FEAT |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 0.796 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | SURFACE TREATMENT PWA 694 COBALT ALLOY; IT TAKES OF THESE TO MAKE UP BLADE SET P/N 4084283 |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.