658213: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include diameter: 14.744 INCHES NOMINAL IN, material: NICKEL ALLOY BLADE, design_type: COMPRESSOR, overall_length: 3.760 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 2840-00-406-8438, 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.
| diameter | 14.744 INCHES NOMINAL IN |
| material | NICKEL ALLOY BLADE |
| design_type | COMPRESSOR |
| overall_length | 3.760 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 | PWA1003 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-00-406-8438 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1003 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| DIAMETER | 14.744 INCHES NOMINAL IN |
| OVERALL LENGTH | 3.760 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY BLADE |
No substitute or cross-reference records for this part.