Flight Control Panel (FCP) is designed and developed for LCA.
It is installed in the cockpit and has been designed to meet the full functional and quadruple redundancy requirements of LCA-FCS (Flight Control System).
The FCP provides the following controls and display to the pilot
Yaw Trim Control in Normal and Emergency Modes
Pitch and Roll Trim Control in Emergency Modes
Normal to Emergency Mode Change Over for Trim Controls
Normal to Standby Gain Change Over for FCS
InitiatePre-flight (P) and Pilot-In-Loop (PL) Built–In–Test (BIT) Results
Visual feedback of BIT results to pilot through GO/ NOGO indicators