4041374: 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: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F100-14, FIG 133, IND 1, 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 2840-00-377-3307, 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 | TITANIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 4 |
| special_features | T.O. 2J-F100-14, FIG 133, IND 1 |
| fsc_application_data | F-15 AIRCRAFT |
| end_item_identification | F100-PW-200 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | CZBJ AND APGF AND CZCJ AND FEAT |
| NSN | 2840-00-377-3307 |
| FSC APPLICATION DATA | F-15 AIRCRAFT |
| STAGE NUMBER | 4 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND APGF AND CZCJ AND FEAT |
| DIAMETER | 16.250 INCHES MINIMUM AND 16.270 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 133, IND 1 |
| END ITEM IDENTIFICATION | F100-PW-200 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.