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Five flight control computers are the heart of the A340 flight control system. They process pilot and autopilot inputs, and function in Normal, Alternate, or Direct flight control laws. 50 Three Flight Control Primary Computers (FCPC) control logic for normal, alternate, and direct flight control laws, speed brake and ground spoiler control, and compute the characteristic speeds displayed on the PFD speed tape. Two Flight Control Secondary Computers (FCSC) manage the direct control law, yaw damping, rudder trim, rudder travel, and rudder pedal travel limits.

Germain) 40 AIRLIlfERTECH aircraft recording system is also handled by the FADECs. As part of the autoflight system in the A340, the thrust levers are also Fly By Wire, and contain no mechanical linkage to the engines. As a result of this, when the Flight Management and Guidance System (FMGS) commands a change in thrust, the thrust levers do not move. Detents in the thrust lever range include Idle, CL (Max Climb Power), MCTIFLX (Maximum Continuous Thrust/Flex Thrust), and TOGA (Takeoff/Go Around Thrust).

When fuel jettison is select- ~ or trim tank as necessary. lmin fuel jettison system. X-FEED valves automatically open. The system is manually activated One of the design points of the through two JETTISON push butA340 was the use of fuel to aid in tons on the overhead fuel control pitch trim and CG optimization. panel. Both push buttons must be Controlling the CG and positioning pressed to begin the operation. it precisely cuts drag dramatically, When this is selected, all crossfeed AIRBUS INDUSTRIE AIRBUS AfJ40 ss Each hydraulic system is controlled via the overhead panel.

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