A combustor for a gas turbine engine comprising a combustion liner defining a combustion chamber, wherein the combustion liner has at least one opening into which a combustor liner mount (200) is received. The combustor liner mount can have at least one cooling passage (208) defined therein having an inlet (210) defining an inlet axis (211) and an outlet (212) defining an outlet axis (213), wherein the inlet axis is not collinear with the outlet axis for providing enhanced cooling to at least one of the combustor liner mount and an adjacent combustion component, such as an igniter or a borescope plug.