9686M18P25: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN, overall_length: 1.720 INCHES MINIMUM AND 1.740 INCHES MAXIMUM IN, special_features: T.O. 2J-TF39-4; TURBINE NOZZLE, material_thickness: 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN, end_item_identification: ACFT ENG TF-39 AND GAS TURBINE ENG LM2500.
This part is cataloged in the U.S. Government catalog under NSN 2840-00-112-2163, 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 |
| stage_number | 2 |
| overall_width | 0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN |
| overall_length | 1.720 INCHES MINIMUM AND 1.740 INCHES MAXIMUM IN |
| special_features | T.O. 2J-TF39-4; TURBINE NOZZLE |
| material_thickness | 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG TF-39 AND GAS TURBINE ENG LM2500 |
| engine_section_location | HIGH PRESSURE TURBINE |
| NSN | 2840-00-112-2163 |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 1.720 INCHES MINIMUM AND 1.740 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| MATERIAL THICKNESS | 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN |
| SPECIAL FEATURES | T.O. 2J-TF39-4; TURBINE NOZZLE |
| END ITEM IDENTIFICATION | ACFT ENG TF-39 AND GAS TURBINE ENG LM2500 |
| MATERIAL | NICKEL ALLOY OVERALL |