3502945: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY, aircraft_location: LOWER FLIGHT CONT PULLEY, aircraft_station_number: 245, side_for_which_designed: RIGHT SIDE, aircraft_mission_design_series: C130-J, material_document_and_classification: MIL-A-21180,A356-T6,CLASS10 MIL SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 3020-01-329-3536, 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 | ALUMINUM ALLOY |
| aircraft_location | LOWER FLIGHT CONT PULLEY |
| aircraft_station_number | 245 |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | C130-J |
| material_document_and_classification | MIL-A-21180,A356-T6,CLASS10 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 3020-01-329-3536 |
| BORE NOMINAL DIAMETER | 1.187 INCHES BOTH ENDS IN |
| HUB NOMINAL DIAMETER | 1.440 INCHES BOTH ENDS IN |
| TEETH QUANTITY | 69 |
| BODY STYLE | WEBBED, SOLID |
| BORE STYLE | PLAIN BOTH ENDS |
| NOMINAL DISTANCE BETWEEN BODY FACE AND PROTRUDING HUB END | 0.128 INCHES BOTH ENDS IN |
| STYLE DESIGNATOR | PROTRUDING HUBS |
| PITCH DIAMETER | 2.5600 INCHES NOMINAL IN |
| HUB STYLE DESIGNATOR | PLAIN BOTH ENDS |
| NOMINAL OUTSIDE DIAMETER | 2.975 INCHES IN |
No substitute or cross-reference records for this part.