5022T04P03: SEAL,METALLIC,AIRCRAFT GAS TURBI.
SEAL,METALLIC,AIRCRAFT GAS TURBI. Key specifications include diameter: 5.298 INCHES MINIMUM AND 5.299 INCHES MAXIMUM IN, material: STEEL LOCATION NOT OTHERWISE SPECIFIED, design_type: AXIAL COMPRESSOR, overall_length: 1.405 INCHES MAXIMUM IN, end_item_identification: TF-34 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-449-8307, 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 | 5.298 INCHES MINIMUM AND 5.299 INCHES MAXIMUM IN |
| material | STEEL LOCATION NOT OTHERWISE SPECIFIED |
| design_type | AXIAL COMPRESSOR |
| overall_length | 1.405 INCHES MAXIMUM IN |
| end_item_identification | TF-34 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-TF34-4, FIG 10, IND 20 |
| criticality_code_justification | ABMZ AND FEAT |
| reference_number_differentiating_characteristics | AS DIFFERENTIATED BY MATERIAL |
| NSN | 2840-01-449-8307 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABMZ AND FEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF34-4, FIG 10, IND 20 |
| DIAMETER | 5.298 INCHES MINIMUM AND 5.299 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.405 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | AIR PURGE SLOTS; THESE SLOTS LOWER THE OPERATING SEAL TEMPERATURE WHICH REDUCES COKING; SEAL IS INTERCHANGEABLE W/P/N 5022T04P02; SEAL WIRE ALLOY CHANGED FROM HAST X TO METALOY 33 FOR IMPROVED DURABILITY |
| END ITEM IDENTIFICATION | TF-34 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | STEEL LOCATION NOT OTHERWISE SPECIFIED |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY MATERIAL |