4079310-01: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: NICKEL ALLOY DISK, design_type: AXIAL COMPRESSOR, stage_number: 10, overall_width: 0.843 INCHES MINIMUM AND 0.851 INCHES MAXIMUM IN, overall_length: 1.671 INCHES NOMINAL IN, special_features: T.O. 2J-F100-54.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-370-9805, 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 DISK |
| design_type | AXIAL COMPRESSOR |
| stage_number | 10 |
| overall_width | 0.843 INCHES MINIMUM AND 0.851 INCHES MAXIMUM IN |
| overall_length | 1.671 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-54 |
| blade_attachment_method | SLOT |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE CORE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-370-9805 |
| STAGE NUMBER | 10 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 1.671 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.843 INCHES MINIMUM AND 0.851 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE CORE |
| MATERIAL | NICKEL ALLOY DISK |