1385M20P01-110B: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 30.000 INCHES NOMINAL IN, material: NICKEL ALLOY BLADE, overall_length: 16.000 INCHES NOMINAL IN, supplementary_features: FOR B MODEL ENGINE, end_item_identification: 2J-F110 ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-476-1478, 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 | 30.000 INCHES NOMINAL IN |
| material | NICKEL ALLOY BLADE |
| stage_number | 9 |
| overall_length | 16.000 INCHES NOMINAL IN |
| supplementary_features | FOR B MODEL ENGINE |
| end_item_identification | 2J-F110 ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | 2J-F110-4,FIG 46,IND 44 |
| criticality_code_justification | AGAV |
| NSN | 2840-01-476-1478 |
| STAGE NUMBER | 9 |
| SUPPLEMENTARY FEATURES | FOR B MODEL ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F110-4,FIG 46,IND 44 |
| DIAMETER | 30.000 INCHES NOMINAL IN |
| OVERALL LENGTH | 16.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | 2J-F110 ENGINE |
| MATERIAL | NICKEL ALLOY BLADE |
No substitute or cross-reference records for this part.