Configuration
112-194-3 is a configuration of a Teledyne engine. It includes a set of components such as a combustor, gas turbine, and starter motor. It is designed to provide efficient power output and reliability when used in an aircraft engine. 112-194-3 is a type of low-bypass turbofan engine typically used in small, light-weight planes. It is characterized by a large fan, a long-stroke turbine and a simple combustor design. This configuration is known for its low fuel consumption, long life, and low operational costs.