284571: SEAL,METALLIC,AIRCRAFT GAS TURBI.
SEAL,METALLIC,AIRCRAFT GAS TURBI. Key specifications include diameter: 4.907 INCHES MINIMUM AND 4.913 INCHES MAXIMUM IN, material: STEEL CORROSION RESISTING OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.090 INCHES MINIMUM AND 0.092 INCHES MAXIMUM IN, special_features: T.O. 2J-J75-4, FIG 31 IN 5; TURBINE ROTOR, FRONT COMPRESSOR DRIVE IN, surface_treatment: CHROMIUM OVERALL.
This part is cataloged in the U.S. Government catalog under NSN 2840-00-547-5564, 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 | 4.907 INCHES MINIMUM AND 4.913 INCHES MAXIMUM IN |
| material | STEEL CORROSION RESISTING OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 0.090 INCHES MINIMUM AND 0.092 INCHES MAXIMUM IN |
| special_features | T.O. 2J-J75-4, FIG 31 IN 5; TURBINE ROTOR, FRONT COMPRESSOR DRIVE IN |
| surface_treatment | CHROMIUM OVERALL |
| end_item_identification | ACFT ENG J75 |
| engine_section_location | TURBINE |
| criticality_code_justification | SFTT AND CZBJ AND ABMZ AND ABHP |
| material_document_and_classification | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME THRUSTRING, TURBINE |
| surface_treatment_document_and_classification | AMS2406 ASSN STD SINGLE TREATMENT RESPONSE OVERALL |
| NSN | 2840-00-547-5564 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS2406 ASSN STD SINGLE TREATMENT RESPONSE OVERALL |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | SFTT AND CZBJ AND ABMZ AND ABHP |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 4.907 INCHES MINIMUM AND 4.913 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.090 INCHES MINIMUM AND 0.092 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-J75-4, FIG 31 IN 5; TURBINE ROTOR, FRONT COMPRESSOR DRIVE IN |
| SURFACE TREATMENT | CHROMIUM OVERALL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME THRUSTRING, TURBINE |
No substitute or cross-reference records for this part.