METHOD FOR BALANCING ROTATING ASSEMBLY OF GAS TURBINE ENGINE

摘要

A method for balancing a rotating assembly (33) of a gas turbine engine (10) includes removing a stator vane (56) from a section of the gas turbine engine. Removing the stator vane provides access to a rotating assembly of the gas turbine engine. The method further includes at least one of adding, removing, and repositioning a weight with respect to the rotating assembly via access to the rotating assembly provided by removing the stator vane.