678604: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY BLADE, design_type: COMPRESSOR, overall_width: 0.536 INCHES NOMINAL IN, overall_length: 2.962 INCHES NOMINAL IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: TF30 AIRCRAFT ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-406-8314, 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 | TITANIUM ALLOY BLADE |
| design_type | COMPRESSOR |
| overall_width | 0.536 INCHES NOMINAL IN |
| overall_length | 2.962 INCHES NOMINAL IN |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | TF30 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | PWA1202 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-00-406-8314 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1202 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| OVERALL LENGTH | 2.962 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.536 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY BLADE |