358214: DISK,COMPRESSOR,AIRCRAFT GAS TUR.
DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: STEEL CORROSION RESISTING OVERALL, bore_shape: STRAIGHT, bore_diameter: 12.00 MILLIMETERS NOMINAL MM, overall_width: 10.0 MILLIMETERS NOMINAL MM, load_direction: RADIAL, surface_finish: GROUND. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-799-0114, 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.
| material | STEEL CORROSION RESISTING OVERALL |
| bore_shape | STRAIGHT |
| bore_diameter | 12.00 MILLIMETERS NOMINAL MM |
| overall_width | 10.0 MILLIMETERS NOMINAL MM |
| load_direction | RADIAL |
| surface_finish | GROUND |
| special_features | RINGS AND BALLS MUST NOT PERMANENTLY CHANGE IN DIMENSION IN EXCESS OF 0.000050 IN./IN. WHEN SUBJECTED TO 600 DEG F FOR 10 HOURS ALSO HARDNESS OF RINGS AND BALLS TO BE RC57 MIN. IN |
| style_designator | NON-LOADING GROOVE, NON-SEPARABLE |
| overall_outside_diameter | 32.00 MILLIMETERS NOMINAL MM |
| internal_fit-up_designation | LOOSE |
| retainer_fabrication_method | PRESSED |
| standard_tolerance_designation | ABEC NO.3 |
| NSN | 2840-00-799-0114 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | WAS DISK,AXIAL COMPRESSOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG TF-33 |
No substitute or cross-reference records for this part.