7033M39P01: BELL CRANK.
The BELL CRANK is a the manufacturer industrial component. Key specifications include material: STEEL CORROSION RESISTING, style_designator: RAISED FACE PIVOT AND END HOLES, features_provided: BEARING, end_hole/ball_diameter: 0.250 INCHES NOMINAL ALL ENDS IN, end_item_identification: ENGINE, AIRCRAFT F101-GE-102., part_name_assigned_by_controlling_agency: BRACKET, BEARING-SELF ALIGNING. This part is cataloged in the U.S.
Government catalog under NSN 3040-01-183-0428, 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 | STEEL CORROSION RESISTING |
| style_designator | RAISED FACE PIVOT AND END HOLES |
| features_provided | BEARING |
| end_hole/ball_diameter | 0.250 INCHES NOMINAL ALL ENDS IN |
| end_item_identification | ENGINE, AIRCRAFT F101-GE-102. |
| part_name_assigned_by_controlling_agency | BRACKET, BEARING-SELF ALIGNING |
| center_to_center_distance_between_fulcrum_and_arm_end_hole/slot/ball | 2.430 INCHES MINIMUM AND 2.450 INCHES MAXIMUM FIRST END IN |
| NSN | 3040-01-183-0428 |
| CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 2.430 INCHES MINIMUM AND 2.450 INCHES MAXIMUM FIRST END IN |
| CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 2.490 INCHES MINIMUM AND 2.510 INCHES MAXIMUM SECOND END IN |
| END HOLE/BALL DIAMETER | 0.250 INCHES NOMINAL ALL ENDS IN |
| STYLE DESIGNATOR | RAISED FACE PIVOT AND END HOLES |
| FEATURES PROVIDED | BEARING |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET, BEARING-SELF ALIGNING |
| END ITEM IDENTIFICATION | ENGINE, AIRCRAFT F101-GE-102. |
| MATERIAL | STEEL CORROSION RESISTING |
No substitute or cross-reference records for this part.