A stator (42) includes a plurality of stator vanes (56) and a shroud (44) operably connected to the stator vanes (56). The shroud (44) includes one or more positioning tabs (70) configured to engage one or more corresponding alignment features (74) of a mating component (40) to radially position the shroud at the mating component (40), the one or more shroud positioning tabs (70) positioning the outer shroud (44) to define a radial tip clearance between an outer shroud (4) and an adjacent rotor (34) of the gas turbine engine.
The present disclosure also extends to a gas turbine engine with a combustor in fluid communication with an assembly of a case and a stator as above.