Patent ID: 8615982

Claim:
A nacelle assembly for an aircraft engine comprising: a fan nozzle movable between a first position and a second position to define a discharge flow area; a thrust reverser movable between a stowed position and an actuated position to divert discharge flow in a thrust reversing direction; an actuator assembly for moving both the fan nozzle and the thrust reverser, the actuator assembly including a first portion coupled to the fan nozzle and a second portion coupled to the thrust reversers, wherein the first portion and the second portion are movable along a common axis and are movable individually for moving the thrust reverser independent of the fan nozzle; wherein the first portion and second portion comprise selectable engageable lugs for selectively engaging and disengaging from the actuator assembly to provide selective independent movement of the fan nozzle and the thrust reverser; an actuator lock preventing movement of the thrust reverser in a locked condition and allowing movement of the thrust reverser in a unlocked condition; and a cowl lock actuateable independent of the actuator lock for preventing movement of the thrust reverser in a locked condition and allowing movement of the thrust reverser in an unlocked condition.