The LP Turbine exit nozzle is located behind the LP turbine rotor assembly and in front of the exhaust frame. Constructed of INCO 738 the forty-eight stationary vanes that make up the exit nozzle straighten core airflow for afterburner use. The forty-eight vanes are divided into six segments of eight, a space equal to a missing vane separates the segments corresponding to the six struts on the exhaust frame. The open space between the segments allows more area for bypass air to mix with core airflow relieving the back pressure on the LP Turbine blades. Relieving the back pressure eliminates the vibration on the blades. The exit nozzle slips over the bore of the exhaust frame and the twelve slotted tabs on the mating flange are aligned with the bolt holes in the rear air seal and exhaust frame. The rear air seal sets between the exhaust frame and the exit nozzle and all three components are held together by twelve bolts with stepped spacers. A tab on the inner flange of the exit nozzle is positioned at the top of the exhaust frame facilitating the proper installation of the exit nozzle with the exhaust frame.