Methods and Criteria for the Balancing of Gas Turbine Rigid Rotors
AS6327
This document establishes process parameters for gas turbine rotor balancing. Adherence to the recommendations made herein will facilitate attainment of the usually high degree of accuracy and precision required for jet engine rotor balance.
Rationale: The EG-1A Balance Committee has recognized the need for a standard to address the people, processes and equipment used in the balancing of aerospace rigid rotors.
