4083150: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 19.448 INCHES NOMINAL IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.664 INCHES NOMINAL IN, special_features: USED ON THE FRONT COMPRESSOR ROTOR AND STATOR ASSEMBLY; REPLACED P/N 4071083, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-451-5473, 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 | 19.448 INCHES NOMINAL IN |
| material | TITANIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 2 |
| overall_length | 0.664 INCHES NOMINAL IN |
| special_features | USED ON THE FRONT COMPRESSOR ROTOR AND STATOR ASSEMBLY; REPLACED P/N 4071083 |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-F100-54, FIG 70, IND 25 |
| criticality_code_justification | CZBJ AND ABHP AND ABMZ AND FEAT |
| material_document_and_classification | PWA1215 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-451-5473 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND ABMZ AND FEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54, FIG 70, IND 25 |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1215 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 19.448 INCHES NOMINAL IN |
| OVERALL LENGTH | 0.664 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | USED ON THE FRONT COMPRESSOR ROTOR AND STATOR ASSEMBLY; REPLACED P/N 4071083 |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |