1498M48P02-110: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 23.095 INCHES MINIMUM AND 23.097 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 1.880 INCHES MINIMUM AND 1.908 INCHES MAXIMUM IN, end_item_identification: F110GE100 ENGINE, engine_section_location: HIGH PRESSURE TURBINE, reference_data_and_literature: 2J-F110-4. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-477-6582, 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 | 23.095 INCHES MINIMUM AND 23.097 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 1.880 INCHES MINIMUM AND 1.908 INCHES MAXIMUM IN |
| end_item_identification | F110GE100 ENGINE |
| engine_section_location | HIGH PRESSURE TURBINE |
| reference_data_and_literature | 2J-F110-4 |
| criticality_code_justification | AGAV |
| NSN | 2840-01-477-6582 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F110-4 |
| DIAMETER | 23.095 INCHES MINIMUM AND 23.097 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.880 INCHES MINIMUM AND 1.908 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| END ITEM IDENTIFICATION | F110GE100 ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.