4081506: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 2.919 INCHES MINIMUM AND 2.929 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-54, end_item_identification: F100PW229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-423-8133, 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 OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 6 |
| overall_length | 2.919 INCHES MINIMUM AND 2.929 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-54 |
| end_item_identification | F100PW229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | CZBJ AND FEAT AND AGAV |
| material_document_and_classification | PWA1202 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-423-8133 |
| STAGE NUMBER | 6 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND FEAT AND AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1202 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 2.919 INCHES MINIMUM AND 2.929 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.