555211: CASE,COMBUSTION CHAMBER,AIRCRAFT.
CASE,COMBUSTION CHAMBER,AIRCRAFT. Key specifications include diameter: 38.438 INCHES MINIMUM AND 38.442 INCHES MAXIMUM IN, design_type: CENTRIFUGAL, overall_length: 6.353 INCHES MINIMUM AND 6.413 INCHES MAXIMUM IN, hardness_rating: 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM OUTER CASE, special_features: ORIGINAL NAME CASE,CENTRIFUGAL COMPRESSOR,TURBINE ENGINE, precious_material: SILVER. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-185-3554, 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 | 38.438 INCHES MINIMUM AND 38.442 INCHES MAXIMUM IN |
| design_type | CENTRIFUGAL |
| overall_length | 6.353 INCHES MINIMUM AND 6.413 INCHES MAXIMUM IN |
| hardness_rating | 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM OUTER CASE |
| special_features | ORIGINAL NAME CASE,CENTRIFUGAL COMPRESSOR,TURBINE ENGINE |
| precious_material | SILVER |
| end_item_identification | ACFT ENG J57 |
| engine_section_location | COMPRESSOR |
| NSN | 2840-00-185-3554 |
| DESIGN TYPE | CENTRIFUGAL |
| PRECIOUS MATERIAL | SILVER |
| HARDNESS RATING | 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM OUTER CASE |
| DIAMETER | 38.438 INCHES MINIMUM AND 38.442 INCHES MAXIMUM IN |
| OVERALL LENGTH | 6.353 INCHES MINIMUM AND 6.413 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME CASE,CENTRIFUGAL COMPRESSOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG J57 |