643E406G9: LINER,COMBUSTION CHAMBER,AIRCRAF.
LINER,COMBUSTION CHAMBER,AIRCRAF. Key specifications include overall_length: 12.030 INCHES MINIMUM AND 12.080 INCHES MAXIMUM IN, special_features: USED ON -7B, -11A, -11B AND -19 SERIES ENGINES A, end_item_identification: J-79 AIRCRAFT TURBINE ENGINES, engine_section_location: COMBUSTION CHAMBER, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-015-1751, 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.
| overall_length | 12.030 INCHES MINIMUM AND 12.080 INCHES MAXIMUM IN |
| special_features | USED ON -7B, -11A, -11B AND -19 SERIES ENGINES A |
| end_item_identification | J-79 AIRCRAFT TURBINE ENGINES |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | AGAV |
| NSN | 2840-01-015-1751 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 12.030 INCHES MINIMUM AND 12.080 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| SPECIAL FEATURES | USED ON -7B, -11A, -11B AND -19 SERIES ENGINES A |
| END ITEM IDENTIFICATION | J-79 AIRCRAFT TURBINE ENGINES |
No substitute or cross-reference records for this part.