A51C33500-1: BELL CRANK.
The BELL CRANK is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, bore_length: 2.093 INCHES MINIMUM AND 2.103 INCHES MAXIMUM IN, bore_diameter: 0.7488 INCHES MINIMUM AND 0.7493 INCHES MAXIMUM IN, style_designator: CLEVIS ENDS, surface_treatment: ANODIZE, fsc_application_data: FLIGHT CONTROL SYSTEM,ACFT. This part is cataloged in the U.S.
Government catalog under NSN 3040-00-008-5375, 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 | 2.093 INCHES MINIMUM AND 2.103 INCHES MAXIMUM IN |
| bore_diameter | 0.7488 INCHES MINIMUM AND 0.7493 INCHES MAXIMUM IN |
| style_designator | CLEVIS ENDS |
| surface_treatment | ANODIZE |
| fsc_application_data | FLIGHT CONTROL SYSTEM,ACFT |
| end_hole/ball_diameter | 0.2497 INCHES MINIMUM AND 0.2507 INCHES MAXIMUM SECOND END IN |
| criticality_code_justification | ABXV AND CZLN |
| center_to_center_distance_between_fulcrum_and_arm_end_hole/slot/ball | 5.234 INCHES NOMINAL SECOND END IN |
| NSN | 3040-00-008-5375 |
| CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 4.765 INCHES NOMINAL FIRST END IN |
| CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 5.234 INCHES NOMINAL SECOND END IN |
| END HOLE/BALL DIAMETER | 0.2497 INCHES MINIMUM AND 0.2507 INCHES MAXIMUM FIRST END IN |
| END HOLE/BALL DIAMETER | 0.2497 INCHES MINIMUM AND 0.2507 INCHES MAXIMUM SECOND END IN |
| FSC APPLICATION DATA | FLIGHT CONTROL SYSTEM,ACFT |
| BORE LENGTH | 2.093 INCHES MINIMUM AND 2.103 INCHES MAXIMUM IN |
| CRITICALITY CODE JUSTIFICATION | ABXV AND CZLN |
| STYLE DESIGNATOR | CLEVIS ENDS |
| SURFACE TREATMENT | ANODIZE |
| BORE DIAMETER | 0.7488 INCHES MINIMUM AND 0.7493 INCHES MAXIMUM IN |
No substitute or cross-reference records for this part.