2840PL0711185: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: NICKEL ALLOY BLADE, design_type: AXIAL COMPRESSOR, overall_length: 2.144 INCHES NOMINAL IN, blade_attachment_method: FIR TREE, end_item_identification: ACFT ENG F100, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-371-1352, 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 | AXIAL COMPRESSOR |
| stage_number | 8 |
| overall_length | 2.144 INCHES NOMINAL IN |
| blade_attachment_method | FIR TREE |
| end_item_identification | ACFT ENG F100 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-371-1352 |
| STAGE NUMBER | 8 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 2.144 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | ACFT ENG F100 |
| MATERIAL | NICKEL ALLOY BLADE |