Gibraltar 7A-B7 Mach.-g Rod End 3/4-10 Male Thread Alloy Steel

Product Description

The GIBRALTAR 7A-B7 MACH.-G is a male-threaded rod end with an eye hole head, manufactured from grade 4140 alloy steel with a black oxide finish. Rod ends of this type serve as pivoting linkage connectors in mechanical assemblies, allowing controlled rotational movement at the joint. The 3/4-10 external male thread engages directly into a clevis, bracket, or actuator rod. The black oxide coating provides mild corrosion resistance and reduces surface reflectivity. This part is installed by millwrights, maintenance mechanics, and industrial technicians working on linkage systems, control rods, and mechanical actuators.

This rod end is suited for industrial and mechanical applications where a threaded male shank must connect to a pivot point or pin-mounted bracket. Typical install scenarios include machine linkages, steering assemblies, industrial automation equipment, and control rod systems. The eye hole head accepts a clevis pin through the 3/4-inch hole diameter, allowing articulation at the connection point. It is sized for moderate-load applications using inch-standard fastener and measurement conventions.

Key Features

• 3/4-10 external male thread for direct engagement into threaded rod or clevis hardware
• Grade 4140 alloy steel construction for strength in mechanical linkage service
• Black oxide finish for mild corrosion resistance and reduced surface glare
• Eye hole head with 3/4-inch hole diameter accepts standard clevis pins
• 1-1/2-inch head outside diameter with 3/4-inch head thickness
• 2-5/8-inch thread length provides substantial engagement depth

Compatibility

Designed as an OEM-style replacement or direct-fit component for mechanical linkage assemblies using 3/4-10 inch-standard threaded rod ends with male external thread configuration.

Installation Notes

Installation is typically performed by licensed millwrights or qualified maintenance mechanics. De-energize and lock out all mechanical, hydraulic, or pneumatic power to the assembly before removing or installing any linkage component. Verify thread engagement depth meets applicable machinery and structural standards before placing the assembly under load. Inspect the clevis pin and retaining hardware for wear before reassembly.