246738: SEAL,METALLIC,AIRCRAFT GAS TURBI.
SEAL,METALLIC,AIRCRAFT GAS TURBI. Key specifications include diameter: 7.070 INCHES MINIMUM AND 7.090 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.693 INCHES MINIMUM AND 0.695 INCHES MAXIMUM IN, special_features: T.O. 2J-J57-24, FIG 16, IND 18; USED ON THE J57-P-21B & 23B ENGINES; REAR ROTOR COMPRESSOR, surface_treatment: CHROMIUM OVERALL.
This part is cataloged in the U.S. Government catalog under NSN 2840-00-505-9305, 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 | 7.070 INCHES MINIMUM AND 7.090 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 0.693 INCHES MINIMUM AND 0.695 INCHES MAXIMUM IN |
| special_features | T.O. 2J-J57-24, FIG 16, IND 18; USED ON THE J57-P-21B & 23B ENGINES; REAR ROTOR COMPRESSOR |
| surface_treatment | CHROMIUM OVERALL |
| end_item_identification | J-57 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | SFTT AND CZBJ AND ABMZ AND ABHP |
| material_document_and_classification | AMS6322 ASSN STD SINGLE MATERIAL RESPONSE OR AAMS6323 ASSN STD 2ND MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME PLATE,BEARING SEAL |
| surface_treatment_document_and_classification | AMS2406 ASSN STD SINGLE TREATMENT RESPONSE OVERALL |
| NSN | 2840-00-505-9305 |
| 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 | AMS6322 ASSN STD SINGLE MATERIAL RESPONSE OR AAMS6323 ASSN STD 2ND MATERIAL RESPONSE OVERALL |
| DIAMETER | 7.070 INCHES MINIMUM AND 7.090 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.693 INCHES MINIMUM AND 0.695 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-J57-24, FIG 16, IND 18; USED ON THE J57-P-21B & 23B ENGINES; REAR ROTOR COMPRESSOR |
| SURFACE TREATMENT | CHROMIUM OVERALL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME PLATE,BEARING SEAL |