108R818P4: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY OVERALL, design_type: COMPRESSOR, overall_length: 16.600 INCHES MINIMUM AND 16.800 INCHES MAXIMUM IN, end_item_identification: GAS TURBINE AND JET ENG ACFTS, engine_section_location: COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-083-6920, 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 | COMPRESSOR |
| overall_length | 16.600 INCHES MINIMUM AND 16.800 INCHES MAXIMUM IN |
| end_item_identification | GAS TURBINE AND JET ENG ACFTS |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-00-083-6920 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 16.600 INCHES MINIMUM AND 16.800 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | GAS TURBINE AND JET ENG ACFTS |
| MATERIAL | TITANIUM ALLOY OVERALL |