74A660635-1001: BELL CRANK.
The BELL CRANK is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, style_designator: CLEVIS, TONGUE, fsc_application_data: AIRCRAFT MODEL FUSELAGE SECTION, end_hole/ball_diameter: 0.375 INCHES NOMINAL FIRST END IN, center_to_center_distance_between_fulcrum_and_arm_end_hole/slot/ball: 6.205 INCHES NOMINAL SECOND END IN. This part is cataloged in the U.S.
Government catalog under NSN 1680-01-142-9050, 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 |
| style_designator | CLEVIS, TONGUE |
| fsc_application_data | AIRCRAFT MODEL FUSELAGE SECTION |
| end_hole/ball_diameter | 0.375 INCHES NOMINAL FIRST END IN |
| center_to_center_distance_between_fulcrum_and_arm_end_hole/slot/ball | 6.205 INCHES NOMINAL SECOND END IN |
| NSN | 1680-01-142-9050 |
| CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 3.387 INCHES NOMINAL FIRST END IN |
| CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 6.205 INCHES NOMINAL SECOND END IN |
| END HOLE/BALL DIAMETER | 0.375 INCHES NOMINAL FIRST END IN |
| FSC APPLICATION DATA | AIRCRAFT MODEL FUSELAGE SECTION |
| STYLE DESIGNATOR | CLEVIS, TONGUE |
| MATERIAL | ALUMINUM ALLOY |
No substitute or cross-reference records for this part.