ACTUATION SYSTEM FOR A THRUST REVERSER OF AN AIRCRAFT PROPULSION SYSTEM

An assembly (66) is provided for an aircraft propulsion system (20). This assembly (66) includes a first actuator (68), a second actuator (68) and a linkage system (70, 72). The linkage system (70, 72) is configured to transfer torque between the first actuator (68) and the second actuator (68). The linkage system (70, 72) includes a first linkage shaft (90), a second linkage shaft (90) and a gearbox (92). The first linkage shaft (90) has a first centerline (94). The second linkage shaft (90) has a second centerline (94) offset from the first centerline (94). The gearbox (92) is coupled to and is between the first linkage shaft (90) and the second linkage shaft (90).