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|