System for locking aircraft engine mounting rod in clevis joint comprises plates which fit between ends of rod and nut and bolt head, plates having studs which fit into bores in rod ends to fix them in position

摘要

The system for locking an aircraft engine mounting rod (20) in a clevis joint (21, 22) comprises plates (25, 26) which fit between the ends of the rod and a nut and bolt head (24). The plates have studs (27) which fit into bores (29, 30) in the rod ends to fix them in position.