9687M92G14: SUPPORT,TURBINE NOZZLE,AIRCRAFT.
SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: STEEL, overall_length: 12.568 INCHES NOMINAL IN, inside_diameter: 25.035 INCHES MINIMUM AND 25.055 INCHES MAXIMUM IN, outside_diameter: 28.233 INCHES NOMINAL IN, mounting_hole_diameter: 0.345 INCHES MINIMUM AND 0.346 INCHES MAXIMUM IN, mounting_hole_quantity: 32. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-563-9154, 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 | STEEL |
| overall_length | 12.568 INCHES NOMINAL IN |
| inside_diameter | 25.035 INCHES MINIMUM AND 25.055 INCHES MAXIMUM IN |
| outside_diameter | 28.233 INCHES NOMINAL IN |
| mounting_hole_diameter | 0.345 INCHES MINIMUM AND 0.346 INCHES MAXIMUM IN |
| mounting_hole_quantity | 32 |
| end_item_identification | ENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE1A |
| criticality_code_justification | AGAV |
| NSN | 2840-00-563-9154 |
| MOUNTING HOLE QUANTITY | 32 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MOUNTING HOLE DIAMETER | 0.345 INCHES MINIMUM AND 0.346 INCHES MAXIMUM IN |
| OVERALL LENGTH | 12.568 INCHES NOMINAL IN |
| OUTSIDE DIAMETER | 28.233 INCHES NOMINAL IN |
| INSIDE DIAMETER | 25.035 INCHES MINIMUM AND 25.055 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | ENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE1A |
| MATERIAL | STEEL |