Flight Control System

The Flight Control System includes:

Primary flight control surfaces - ailerons, twin rudders, differential/collective leading edge flaps, differential/collective trailing edge flaps and differential/ collective stabilators
The controls - stick, rudder pedals, flap elector switch.
Flight Control Computers - Two duplicate computers, A and B
Hydraulic Actuators operated by dual Hydraulic Systems
Electrical and Mechanical backup controls.

Further information: