4046565: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 16.270 INCHES MINIMUM AND 16.290 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 0.135 INCHES MINIMUM AND 0.155 INCHES MAXIMUM IN, overall_length: 0.185 INCHES MINIMUM AND 0.195 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-14, FIG 134, IND 1.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-013-1599, 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 | 16.270 INCHES MINIMUM AND 16.290 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 5 |
| overall_width | 0.135 INCHES MINIMUM AND 0.155 INCHES MAXIMUM IN |
| overall_length | 0.185 INCHES MINIMUM AND 0.195 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-14, FIG 134, IND 1 |
| fsc_application_data | F-15 AIRCRAFT |
| end_item_identification | ENGINE,AIRCRAFT,TURBOFAN,MODEL NO. F100/PW/100 |
| engine_section_location | COMPRESSOR |
| NSN | 2840-01-013-1599 |
| FSC APPLICATION DATA | F-15 AIRCRAFT |
| STAGE NUMBER | 5 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| DIAMETER | 16.270 INCHES MINIMUM AND 16.290 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.185 INCHES MINIMUM AND 0.195 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.135 INCHES MINIMUM AND 0.155 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 134, IND 1 |
| END ITEM IDENTIFICATION | ENGINE,AIRCRAFT,TURBOFAN,MODEL NO. F100/PW/100 |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.