4083880-01: COMPRESSOR,AIRCRAFT GAS TURBINE.
COMPRESSOR,AIRCRAFT GAS TURBINE. Key specifications include diameter: 21.935 INCHES MINIMUM AND 21.942 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 6.669 INCHES MINIMUM AND 6.679 INCHES MAXIMUM IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE/CORE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-369-6008, 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 | 21.935 INCHES MINIMUM AND 21.942 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 6.669 INCHES MINIMUM AND 6.679 INCHES MAXIMUM IN |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE/CORE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-369-6008 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 21.935 INCHES MINIMUM AND 21.942 INCHES MAXIMUM IN |
| OVERALL LENGTH | 6.669 INCHES MINIMUM AND 6.679 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE/CORE |
| MATERIAL | NICKEL ALLOY OVERALL |