555665: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 24.900 INCHES NOMINAL IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, stage_number: 10, overall_length: 1.134 INCHES MINIMUM AND 1.154 INCHES MAXIMUM IN, hardness_rating: 30.0 ROCKWELL C NOMINAL OVERALL. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-227-8889, 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 | 24.900 INCHES NOMINAL IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 10 |
| overall_length | 1.134 INCHES MINIMUM AND 1.154 INCHES MAXIMUM IN |
| hardness_rating | 30.0 ROCKWELL C NOMINAL OVERALL |
| special_features | T.O. 2J-J75-4, FIG 13, IND 12; CASE-REAR COMPRESSOR FRONT |
| surface_treatment | NICKEL AND CADMIUM OVERALL |
| end_item_identification | J-75 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | CZBJ AND SFTT AND ABMZ AND ABHP AND FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME RING,COMPRESSOR ROTOR,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-00-227-8889 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS2416 ASSN STD SINGLE TREATMENT RESPONSE OVERALL |
| STAGE NUMBER | 10 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| HARDNESS RATING | 30.0 ROCKWELL C NOMINAL OVERALL |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND SFTT AND ABMZ AND ABHP AND FEAT |
| DIAMETER | 24.900 INCHES NOMINAL IN |
| OVERALL LENGTH | 1.134 INCHES MINIMUM AND 1.154 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-J75-4, FIG 13, IND 12; CASE-REAR COMPRESSOR FRONT |
| SURFACE TREATMENT | NICKEL AND CADMIUM OVERALL |