9103M20G08: CASE,COMBUSTION CHAMBER,AIRCRAFT.
CASE,COMBUSTION CHAMBER,AIRCRAFT. Key specifications include diameter: 28.600 INCHES NOMINAL IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, end_item_identification: ACFT ENG TF39, engine_section_location: COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-035-9078, 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 | 28.600 INCHES NOMINAL IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| end_item_identification | ACFT ENG TF39 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-035-9078 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 28.600 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.