1522M89P04: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 14.403 INCHES MINIMUM AND 14.407 INCHES MAXIMUM IN, overall_width: 0.331 INCHES NOMINAL IN, overall_length: 1.661 INCHES NOMINAL IN, end_item_identification: F110GE100 AIRCRAFT ENGINE, engine_section_location: HIGH PRESSURE TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-322-4571, 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 | 14.403 INCHES MINIMUM AND 14.407 INCHES MAXIMUM IN |
| overall_width | 0.331 INCHES NOMINAL IN |
| overall_length | 1.661 INCHES NOMINAL IN |
| end_item_identification | F110GE100 AIRCRAFT ENGINE |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-322-4571 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 14.403 INCHES MINIMUM AND 14.407 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.661 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.331 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| END ITEM IDENTIFICATION | F110GE100 AIRCRAFT ENGINE |