Flight Director & Course Control System

Flight Director & Course Control System forms the core course-reference, command indication, and control-signal coordination architecture of the Mi-8 and Mi-17 helicopter family. This subsystem includes course receivers, control and processing blocks, command and indication units, interface and matching modules, signal amplification and filtering devices used for generation, conversion, verification, and visual presentation of course and flight-director data in the cockpit. The system ensures correct formation of course commands, controlled switching of operating modes, stable interaction between sensors, processing logic, and pilot indication, as well as reliable transmission of guidance information to flight control and stabilization systems. This subsystem operates as an integrated part of the helicopter avionics and automatic control architecture, supporting pilot orientation, system logic coordination, and command-signal distribution during all phases of flight. Flight director and course control equipment is engineered for continuous operation under vibration exposure, temperature fluctuations, electrical load instability, and long-duty helicopter flight cycles. This category is applied during scheduled maintenance, avionics recovery, cockpit modernization, system upgrade programs, and fleet-level technical support. All units are supplied in New, Overhauled, or Serviceable condition, with verified traceability and full technical documentation available upon request. Fast international dispatch from UAE and EU stock hubs ensures stable logistics support for MRO companies, fleet operators, and aviation trading organizations.