A method of applying a profiled abradable 
coating onto a substrate in which an abradable 
ceramic coating composition is applied to a 
metal substrate using one or more 
coating application techniques to produce a defined 
ceramic pattern without requiring a separate web or grid to be brazed onto the substrate. The invention is particularly designed to withstand the higher operating temperatures encountered with the stage 1 section of 7FA+e 
gas turbines to allow for increased coating life without significant deterioration in structural or 
functional integrity. Typically, the 
grid pattern coating begins approximately 0.431″ after the 
leading edge of the shroud, and ends approximately 1.60″ before the 
trailing edge of the shroud. In the case of 
diamond-shaped patterns, the 
grid pattern will be about 0.28″ long and 0.28″ wide, with an overall thickness of about 0.46.″ The coatings thus provide the required levels of abradability and leakage performance and may be applied as a chevron or 
diamond pattern with the shape oriented such that the diagonals run perpendicular and parallel to the sides of the shroud.