4041378: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 16.250 INCHES MINIMUM AND 16.270 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F100-14, FIG 136, IND 14, fsc_application_data: F-15 AIRCRAFT, end_item_identification: F100-PW-200 AIRCRAFT ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-00-377-3310, 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 | 16.250 INCHES MINIMUM AND 16.270 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 8 |
| special_features | T.O. 2J-F100-14, FIG 136, IND 14 |
| fsc_application_data | F-15 AIRCRAFT |
| end_item_identification | F100-PW-200 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| NSN | 2840-00-377-3310 |
| FSC APPLICATION DATA | F-15 AIRCRAFT |
| STAGE NUMBER | 8 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| DIAMETER | 16.250 INCHES MINIMUM AND 16.270 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 136, IND 14 |
| END ITEM IDENTIFICATION | F100-PW-200 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.