4081507: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY BLADE, design_type: AXIAL COMPRESSOR, overall_width: 0.674 INCHES NOMINAL IN, overall_length: 2.936 INCHES NOMINAL IN, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-418-9485, 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 | AXIAL COMPRESSOR |
| stage_number | 7 |
| overall_width | 0.674 INCHES NOMINAL IN |
| overall_length | 2.936 INCHES NOMINAL IN |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | CZBJ AND ABHP AND ABMK |
| material_document_and_classification | PWA1209 MFR REF SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-01-418-9485 |
| STAGE NUMBER | 7 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND ABMK |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1209 MFR REF SINGLE MATERIAL RESPONSE BLADE |
| OVERALL LENGTH | 2.936 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.674 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | TITANIUM ALLOY BLADE |