1864M75: CASE,COMBUSTION CHAMBER,AIRCRAFT.
CASE,COMBUSTION CHAMBER,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F110-4, FIG 65; COMBUSTION DIFFUSER NOZZLE, end_item_identification: F110-100 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMBUSTION CHAMBER, criticality_code_justification: CZBJ AND FEAT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-426-4379, 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 |
| special_features | T.O. 2J-F110-4, FIG 65; COMBUSTION DIFFUSER NOZZLE |
| end_item_identification | F110-100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | CZBJ AND FEAT |
| NSN | 2840-01-426-4379 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND FEAT |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| SPECIAL FEATURES | T.O. 2J-F110-4, FIG 65; COMBUSTION DIFFUSER NOZZLE |
| END ITEM IDENTIFICATION | F110-100 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.