2195427: GUIDE,COMBUSTION CHAMBER,TURBINE.
GUIDE,COMBUSTION CHAMBER,TURBINE. Key specifications include material: NICKEL ALLOY, overall_width: 1.890 INCHES MINIMUM AND 1.930 INCHES MAXIMUM IN, overall_diameter: 7.451 INCHES MINIMUM AND 7.461 INCHES MAXIMUM IN, end_item_identification: TF-30 AIRCRAFT ENGINE, criticality_code_justification: MATT AND ADAV AND ABMK AND AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-350-4823, 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 |
| overall_width | 1.890 INCHES MINIMUM AND 1.930 INCHES MAXIMUM IN |
| overall_diameter | 7.451 INCHES MINIMUM AND 7.461 INCHES MAXIMUM IN |
| end_item_identification | TF-30 AIRCRAFT ENGINE |
| criticality_code_justification | MATT AND ADAV AND ABMK AND AGAV |
| NSN | 2840-01-350-4823 |
| OVERALL DIAMETER | 7.451 INCHES MINIMUM AND 7.461 INCHES MAXIMUM IN |
| CRITICALITY CODE JUSTIFICATION | MATT AND ADAV AND ABMK AND AGAV |
| OVERALL WIDTH | 1.890 INCHES MINIMUM AND 1.930 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | TF-30 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY |
No substitute or cross-reference records for this part.