1386M12G09: CASE,COMBUSTION CHAMBER,AIRCRAFT.
CASE,COMBUSTION CHAMBER,AIRCRAFT. Key specifications include material: NICKEL ALLOY OUTER CASE, design_type: AXIAL COMPRESSOR, overall_length: 32.882 INCHES NOMINAL IN, end_item_identification: ACFT ENG F110, engine_section_location: COMBUSTION CHAMBER, reference_data_and_literature: 2J-F110-14 FIG 69 IND 16. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-423-8147, 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 OUTER CASE |
| design_type | AXIAL COMPRESSOR |
| overall_length | 32.882 INCHES NOMINAL IN |
| end_item_identification | ACFT ENG F110 |
| engine_section_location | COMBUSTION CHAMBER |
| reference_data_and_literature | 2J-F110-14 FIG 69 IND 16 |
| NSN | 2840-01-423-8147 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| REFERENCE DATA AND LITERATURE | 2J-F110-14 FIG 69 IND 16 |
| OVERALL LENGTH | 32.882 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| MATERIAL | NICKEL ALLOY OUTER CASE |
No substitute or cross-reference records for this part.