1461M87G18: FRAME,TURBINE,AIRCRAFT GAS TURBI.
FRAME,TURBINE,AIRCRAFT GAS TURBI. Key specifications include material: CHROMIUM ALLOY, overall_length: 6.500 INCHES NOMINAL IN, inside_diameter: 16.778 INCHES NOMINAL IN, outside_diameter: 32.000 INCHES NOMINAL IN, end_item_identification: F110-GE-129 ENGINE, reference_data_and_literature: 2J-F110-4. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-477-9257, 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 | CHROMIUM ALLOY |
| overall_length | 6.500 INCHES NOMINAL IN |
| inside_diameter | 16.778 INCHES NOMINAL IN |
| outside_diameter | 32.000 INCHES NOMINAL IN |
| end_item_identification | F110-GE-129 ENGINE |
| reference_data_and_literature | 2J-F110-4 |
| criticality_code_justification | AGAV |
| number_of_variable_guide_vanes | 10 |
| NSN | 2840-01-477-9257 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F110-4 |
| OVERALL LENGTH | 6.500 INCHES NOMINAL IN |
| OUTSIDE DIAMETER | 32.000 INCHES NOMINAL IN |
| NUMBER OF VARIABLE GUIDE VANES | 10 |
| INSIDE DIAMETER | 16.778 INCHES NOMINAL IN |
| END ITEM IDENTIFICATION | F110-GE-129 ENGINE |
| MATERIAL | CHROMIUM ALLOY |
No substitute or cross-reference records for this part.