Engine control panel ПУД-50А is intended for remote control of aircraft engines in the following modes:
|remote differential electric control of operation of two engines using two TCLs
|remote electric control of operation of two engines with automatic thrust control (ATC) by signals from the integrated control system (ICS)
Information exchange with aircraft ICS is provided via code communication lines in ARINC429 format.
Components of panel ПУД-50А:
|electrical actuator (throttle control) СГ ПУД-50А
|electronic control unit БУП ПУД-50А
|mounting frame РМ БУП ПУД-50