1864M75G01-110: CASE,COMBUSTION CHAMBER,AIRCRAFT.
CASE,COMBUSTION CHAMBER,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, end_item_identification: F110, engine_section_location: COMBUSTION CHAMBER, reference_data_and_literature: 2J-F110-4 FIG2 IND 49, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-506-0348, 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.
| design_type | AXIAL COMPRESSOR |
| end_item_identification | F110 |
| engine_section_location | COMBUSTION CHAMBER |
| reference_data_and_literature | 2J-F110-4 FIG2 IND 49 |
| criticality_code_justification | AGAV |
| NSN | 2840-01-506-0348 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F110-4 FIG2 IND 49 |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| END ITEM IDENTIFICATION | F110 |