4066528: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 12.370 INCHES MINIMUM AND 12.380 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 2.075 INCHES MINIMUM AND 2.085 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-14, FIG 130, IND 20, fsc_application_data: F-15 AIRCRAFT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-243-2472, 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 | 12.370 INCHES MINIMUM AND 12.380 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 2.075 INCHES MINIMUM AND 2.085 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-14, FIG 130, IND 20 |
| fsc_application_data | F-15 AIRCRAFT |
| end_item_identification | F100-PW-200/220 ACFT ENGINES |
| engine_section_location | DIFFUSER |
| criticality_code_justification | ABHP AND ABMZ AND APGF AND CZBJ AND FEAT |
| NSN | 2840-01-243-2472 |
| FSC APPLICATION DATA | F-15 AIRCRAFT |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND APGF AND CZBJ AND FEAT |
| DIAMETER | 12.370 INCHES MINIMUM AND 12.380 INCHES MAXIMUM IN |
| OVERALL LENGTH | 2.075 INCHES MINIMUM AND 2.085 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | DIFFUSER |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 130, IND 20 |
| END ITEM IDENTIFICATION | F100-PW-200/220 ACFT ENGINES |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.