4074047: LINER,COMBUSTION CHAMBER,AIRCRAF.
LINER,COMBUSTION CHAMBER,AIRCRAF. Key specifications include diameter: 24.178 INCHES MINIMUM AND 24.198 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN, material_thickness: 0.040 INCHES MINIMUM AND 0.055 INCHES MAXIMUM IN, end_item_identification: F100/200 ENG CORE MODULE, engine_section_location: COMBUSTION CHAMBER. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-365-0139, 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 | 24.178 INCHES MINIMUM AND 24.198 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN |
| material_thickness | 0.040 INCHES MINIMUM AND 0.055 INCHES MAXIMUM IN |
| end_item_identification | F100/200 ENG CORE MODULE |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | AGAV |
| NSN | 2840-01-365-0139 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 24.178 INCHES MINIMUM AND 24.198 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| MATERIAL THICKNESS | 0.040 INCHES MINIMUM AND 0.055 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | F100/200 ENG CORE MODULE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.