
An exhaust flap for use in the exhaust section of an aircraft gas turbine engine is built with increased service life and ease of replacement. The exhaust flap includes convergent nozzle flaps, divergent nozzle flaps, convergent seal flaps and divergent seal flaps. The exhaust flap comprises a frame assembly with means for mounting in the engine and effecting its movement. The frame assembly is particularly characterized in having an open frame with at least one rail having a receiving channel. ...











