Provided is a brake rod assembly for an aircraft landing gear. The brake rod assembly comprises: a support member (301); a first brake rod (303, 305) comprising a first pivot point (306) and a second pivot point (304); and a second brake rod (302), characterised in that the support member is coupled to the first pivot point and the second brake rod is coupled to the second pivot point; and the first and second pivot points are longitudinally spaced apart along a first portion (305) of the first brake rod.