123CM12006-501: BELL CRANK.
The BELL CRANK is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, bore_length: 1.937 INCHES MINIMUM AND 1.947 INCHES MAXIMUM IN, bore_diameter: 0.811 INCHES MINIMUM AND 0.812 INCHES MAXIMUM IN, style_designator: CLEVIS ENDS, surface_treatment: ANODIZE, end_hole/ball_diameter: 0.312 INCHES MINIMUM AND 0.313 INCHES MAXIMUM FIRST END IN. This part is cataloged in the U.S.
Government catalog under NSN 1680-00-009-9118, 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 |
| bore_length | 1.937 INCHES MINIMUM AND 1.947 INCHES MAXIMUM IN |
| bore_diameter | 0.811 INCHES MINIMUM AND 0.812 INCHES MAXIMUM IN |
| style_designator | CLEVIS ENDS |
| surface_treatment | ANODIZE |
| end_hole/ball_diameter | 0.312 INCHES MINIMUM AND 0.313 INCHES MAXIMUM FIRST END IN |
| end_item_identification | E-2C AIRCRAFT |
| center_to_center_distance_between_fulcrum_and_arm_end_hole/slot/ball | 5.000 INCHES NOMINAL FIRST END IN |
| NSN | 1680-00-009-9118 |
| CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 5.000 INCHES NOMINAL FIRST END IN |
| CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 5.992 INCHES NOMINAL SECOND END IN |
| END HOLE/BALL DIAMETER | 0.312 INCHES MINIMUM AND 0.313 INCHES MAXIMUM FIRST END IN |
| END HOLE/BALL DIAMETER | 0.249 INCHES MINIMUM AND 0.251 INCHES MAXIMUM SECOND END IN |
| BORE LENGTH | 1.937 INCHES MINIMUM AND 1.947 INCHES MAXIMUM IN |
| STYLE DESIGNATOR | CLEVIS ENDS |
| SURFACE TREATMENT | ANODIZE |
| END ITEM IDENTIFICATION | E-2C AIRCRAFT |
| BORE DIAMETER | 0.811 INCHES MINIMUM AND 0.812 INCHES MAXIMUM IN |
| MATERIAL | ALUMINUM ALLOY |
No substitute or cross-reference records for this part.