A cooling system for a gas turbine engine turbine section includes a rotor supporting a blade having a cooling passage. A traversing optical path for a measuring beam is formed in the inner chamber. The tuning can be performed by selecting at least one connection area for the component among the at least two of the multiple connection areas. Finally, the locations in an image file of the file systems are determined according to the orders arranged by the access messages so as to compress the file systems into the image file. The host computer is configured for burning extended display identification data for the VGA interface into the liquid crystal display via the print interface, the interface-inverting circuit and the VGA interface, and is configured for burning extended display identification data for the DVI into the liquid crystal display via the print interface, the interface-inverting circuit and the DVI. In an exemplary embodiment, a plurality of fiber-optic members transmit light from one or more individual light sources to corresponding ones of a plurality of individual shower sprays or nozzles.