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A method of assembling a nacelle for a gas turbine engine that includes an inlet end, an exhaust end, and an axis that extends through the engine from the inlet end through the exhaust end is provided. The method includes providing a cowl sized to cover at least a portion of the engine and coupling

A method of assembling a nacelle for a gas turbine engine that includes an inlet end, an exhaust end, and an axis that extends through the engine from the inlet end through the exhaust end is provided. The method includes providing a cowl sized to cover at least a portion of the engine and coupling the cowl to the engine such that the cowl is slideable along the axis toward at least one of the inlet end and the exhaust end.

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1. A method of assembling a nacelle for a gas turbine engine that includes an inlet end, an exhaust end, and an axis that extends through the engine from the inlet end through the exhaust end, said method comprising: providing a fan cowl sized to cover at least a first axial portion of the engine;ex

1. A method of assembling a nacelle for a gas turbine engine that includes an inlet end, an exhaust end, and an axis that extends through the engine from the inlet end through the exhaust end, said method comprising: providing a fan cowl sized to cover at least a first axial portion of the engine;extending the fan cowl about the first axial portion of the engine;extending a transcowl circumferentially about at least a second axial portion of the engine, the fan cowl extending from forward of the transcowl to an overlapping relationship with the transcowl; andcoupling the fan cowl to an engine mounting pylon and the engine such that the fan cowl is movable with respect to the engine along the axis toward at least one of the inlet end and the exhaust end and the transcowl is movable with respect to the engine along the axis toward at least one of the inlet end and the exhaust end, wherein the fan cowl is independently slideable with respect to the transcowl along the axis toward at least one of the inlet end and the exhaust end. 2. A method in accordance with claim 1, further comprising: providing a track; andcoupling the fan cowl to the track such that the fan cowl is slideable along the track. 3. A method in accordance with claim 1, wherein providing a fan cowl sized to cover at least a portion of the engine comprises providing an annular fan cowl that includes a first half and a second half, and wherein coupling the fan cowl to the engine comprises coupling the first half to the second half about the engine. 4. A method in accordance with claim 3, wherein coupling the first half to the second half about the engine comprises coupling the first half to the second half using at least one latch. 5. A method in accordance with claim 3, wherein coupling the first half to the second half about the engine comprises coupling a limit stop between the first half and the second half, the limit stop configured to control a distance that the first half and the second half are separable from one another. 6. A method in accordance with claim 3, wherein coupling the first half to the second half about the engine comprises: providing a mounting assembly; andcoupling the mounting assembly between the first half and the second half, the mounting assembly configured to guide the first half and the second half away from the axis. 7. A method in accordance with claim 6, wherein providing a mounting assembly comprises providing a mounting assembly that includes a rate control device configured to control a rate at which the first half and the second half are moveable relative to one another. 8. A method in accordance with claim 1, wherein providing a fan cowl sized to cover at least a portion of the engine comprises providing an arcuate fan cowl. 9. A method in accordance with claim 1, wherein coupling the fan cowl to the engine comprises coupling the fan cowl and the transcowl to the engine such that the fan cowl overlaps the transcowl, the fan cowl slideable over the transcowl toward the exhaust end. 10. A method in accordance with claim 9, wherein coupling the fan cowl and the transcowl to the engine comprises coupling the fan cowl to the transcowl such that the fan cowl and the transcowl are moveable together. 11. A nacelle for housing an engine that includes an inlet end, an exhaust end, and an axis extending through the engine from the inlet end through the exhaust end, said nacelle comprising: a fan cowl sized to cover at least a first axial portion of the engine, said fan cowl coupled to an engine mounting pylon; anda transcowl circumscribing at least a second axial portion of the engine, said fan cowl extending from forward of said transcowl to an overlapping relationship with said transcowl, said fan cowl movable with respect to the engine along the axis toward at least one of the inlet end and the exhaust end, said transcowl movable with respect to the engine along the axis toward at least one of the inlet end and the exhaust end, said fan cowl independently slideable with respect to said transcowl along the axis toward at least one of the inlet end and the exhaust end. 12. A nacelle in accordance with claim 11, further comprising a track, wherein said fan cowl is coupled to said track such that said fan cowl is slideable along said track. 13. A nacelle in accordance with claim 11, wherein said fan cowl is annular, said fan cowl comprising a first half and a second half that are coupled together about the engine. 14. A nacelle in accordance with claim 13, further comprising at least one latch configured to couple said first half to said second half. 15. A nacelle in accordance with claim 13, further comprising a limit stop coupled between said first half and said second half, said limit stop configured to control a distance that said first half and said second half are separable from one another. 16. A nacelle in accordance with claim 13, further comprising a mounting assembly coupled between said first half and said second half, said mounting assembly configured to guide said first half and said second half away from the axis. 17. A nacelle in accordance with claim 16, wherein said mounting assembly comprises a rate control device configured to control a rate at which said first half and said second half are moveable relative to one another. 18. A nacelle in accordance with claim 11, wherein said fan cowl is arcuate. 19. A nacelle in accordance with claim 11, wherein said fan cowl and said transcowl are configured to be coupled to the engine such that said fan cowl overlaps said transcowl, said fan cowl slideable over said transcowl toward the exhaust end. 20. A nacelle in accordance with claim 19, wherein said fan cowl is coupled to said transcowl such that said fan cowl and said transcowl are moveable together.