658516: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: NICKEL ALLOY BLADE, design_type: COMPRESSOR, overall_width: 0.780 INCHES NOMINAL IN, overall_length: 1.306 INCHES NOMINAL IN, special_features: WAS BLADE,TURBINE ENGINE, material_thickness: 0.470 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-413-0797, 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 | COMPRESSOR |
| overall_width | 0.780 INCHES NOMINAL IN |
| overall_length | 1.306 INCHES NOMINAL IN |
| special_features | WAS BLADE,TURBINE ENGINE |
| material_thickness | 0.470 INCHES NOMINAL IN |
| end_item_identification | TF30 ACFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | PWA1005 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-00-413-0797 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1005 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| OVERALL LENGTH | 1.306 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.780 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL THICKNESS | 0.470 INCHES NOMINAL IN |
| SPECIAL FEATURES | WAS BLADE,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF30 ACFT ENGINE |
| MATERIAL | NICKEL ALLOY BLADE |
No substitute or cross-reference records for this part.