4081609-02: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: NICKEL ALLOY BLADE, design_type: AXIAL COMPRESSOR, overall_width: 0.935 INCHES MINIMUM AND 0.943 INCHES MAXIMUM IN, overall_length: 1.905 INCHES NOMINAL IN, special_features: T.O. 2J-F100-54, blade_attachment_method: SLOT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-370-9804, 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 BLADE |
| design_type | AXIAL COMPRESSOR |
| stage_number | 9 |
| overall_width | 0.935 INCHES MINIMUM AND 0.943 INCHES MAXIMUM IN |
| overall_length | 1.905 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 | 2840-01-370-9804 |
| STAGE NUMBER | 9 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 1.905 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.935 INCHES MINIMUM AND 0.943 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE/CORE |
| MATERIAL | NICKEL ALLOY BLADE |