565507: HUB,COMPRESSOR,AIRCRAFT GAS TURB.
HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include special_features: TITANIUM ALLOY, part_name_assigned_by_controlling_agency: HUB,COMPRESSOR ROTOR,TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 5306-00-558-6122, 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.
| special_features | TITANIUM ALLOY |
| part_name_assigned_by_controlling_agency | HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| NSN | 5306-00-558-6122 |
| HEAD HEIGHT | 0.123 INCHES NOMINAL IN |
| FASTENER LENGTH | 2.092 INCHES NOMINAL IN |
| THREAD LENGTH | 0.410 INCHES MINIMUM IN |
| HARDNESS RATING | 36.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL |
| SHANK UNTHREADED HOLE DIAMETER | 0.068 INCHES NOMINAL FIRST HOLE IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6382 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NOMINAL THREAD DIAMETER | 0.250 INCHES IN |
| FEATURES PROVIDED | FINISHED HEAD |
| HEAD STYLE | HEXAGON |
| THREAD DIRECTION | RIGHT-HAND |
No substitute or cross-reference records for this part.