9526M11G03: SUPPORT,TURBINE NOZZLE,AIRCRAFT.
SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: NICKEL ALLOY, overall_length: 2.407 INCHES NOMINAL IN, inside_diameter: 21.040 INCHES MINIMUM AND 21.050 INCHES MAXIMUM IN, outside_diameter: 24.904 INCHES MINIMUM AND 24.908 INCHES MAXIMUM IN, mounting_hole_diameter: 0.278 INCHES MINIMUM AND 0.287 INCHES MAXIMUM IN, mounting_hole_quantity: 60. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-221-8304, 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_length | 2.407 INCHES NOMINAL IN |
| inside_diameter | 21.040 INCHES MINIMUM AND 21.050 INCHES MAXIMUM IN |
| outside_diameter | 24.904 INCHES MINIMUM AND 24.908 INCHES MAXIMUM IN |
| mounting_hole_diameter | 0.278 INCHES MINIMUM AND 0.287 INCHES MAXIMUM IN |
| mounting_hole_quantity | 60 |
| end_item_identification | ACFT ENG F101-GE-102 |
| NSN | 2840-01-221-8304 |
| MOUNTING HOLE QUANTITY | 60 |
| MOUNTING HOLE DIAMETER | 0.278 INCHES MINIMUM AND 0.287 INCHES MAXIMUM IN |
| OVERALL LENGTH | 2.407 INCHES NOMINAL IN |
| OUTSIDE DIAMETER | 24.904 INCHES MINIMUM AND 24.908 INCHES MAXIMUM IN |
| INSIDE DIAMETER | 21.040 INCHES MINIMUM AND 21.050 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | ACFT ENG F101-GE-102 |
| MATERIAL | NICKEL ALLOY |