The PT6C-67 Series incorporates the latest advanced technologies in the drive to exceed our customers’ expectations in performance, reliability, durability, fuel consumption and environmental friendliness. The 1,200 to 2,000 shaft horsepower class PT6C-67 is based on the PT6A-67 Series airline turboprop engine, extending the inherent benefit of airline dependability to the helicopter market. The PT6C-67 remains a PT6 in basic configuration, with its two-shaft layout consisting of a multi-stage compressor driven by a single-stage compressor turbine and an independent shaft coupling the power turbine to the output shaft. It also incorporates the latest advanced compressor, combustion and turbine technologies to provide an impressive power-to-weight ratio while delivering low fuel consumption, low emissions, high durability and excellent operating economics. With its modern engine control ranging from Electronic Engine Control (EEC) to Full Authority Digital Engine Control (FADEC), the PT6C-67 Series provides ease of pilot operation and enhanced maintenance diagnostics to maximize engine refurbishment intervals.
Single-PT6 power section with direct output drive
- Leveraging the successful PT6A-67 airline turboprop