K350P18: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, design_type: COMPRESSOR, overall_width: 1.696 INCHES NOMINAL IN, overall_length: 6.289 INCHES MINIMUM AND 6.309 INCHES MAXIMUM IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, blade_attachment_method: FIR TREE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-110-5977, 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 | COMPRESSOR |
| stage_number | 3 |
| overall_width | 1.696 INCHES NOMINAL IN |
| overall_length | 6.289 INCHES MINIMUM AND 6.309 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| blade_attachment_method | FIR TREE |
| end_item_identification | TF-39 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-00-110-5977 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 6.289 INCHES MINIMUM AND 6.309 INCHES MAXIMUM IN |
| OVERALL WIDTH | 1.696 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF-39 |
| MATERIAL | STEEL BLADE |