4026508: DUCT,TURBINE,AIRCRAFT GAS TURBIN.
DUCT,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 7.930 INCHES MINIMUM AND 7.950 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 2.235 INCHES MINIMUM AND 2.245 INCHES MAXIMUM IN, end_item_identification: F-100 AIRCRAFT ENGINE, engine_section_location: TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-321-4577, 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 | 7.930 INCHES MINIMUM AND 7.950 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 2.235 INCHES MINIMUM AND 2.245 INCHES MAXIMUM IN |
| end_item_identification | F-100 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-00-321-4577 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 7.930 INCHES MINIMUM AND 7.950 INCHES MAXIMUM IN |
| OVERALL LENGTH | 2.235 INCHES MINIMUM AND 2.245 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| END ITEM IDENTIFICATION | F-100 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.