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In the event of four engine failure, RAT deployment will be automatically controlled by the HSMU to pressurize the Green system. - one handpump on the Yellow system for cargo doors operation when no electrical power is available. 502/90 Issue 6 5. 1 A340 Flight Controls - EFCS Electronic Flight Control System (EFCS) Surfaces : • All hydraulically activated • All electrically controlled • Mechanical back-up control : - Rudder - Trimmable Horizontal Stabilizer (THS). 2 A340 Flight Controls - EFCS General The A340 fly-by-wire system was designed and certificated to make this new aircraft more cost effective, more pleasant to fly, and more comfortable than conventional aircraft.

In manual mode (above 190 KT, in CONF 0) the outboard ailerons are centered. Each spoiler is driven by one electro-hydraulic servo control which is connected to one specific computer. 6°. The rudder is operated by three independent hydraulic servo-controls, with a common mechanical input. This mechanical input receives three commands : - Rudder pedal input limited by the Pedal Travel Limitation Unit (PTLU) ; - Rudder trim actuator electrical input ; - Yaw damper electrical input. The mechanical input is limited by the Travel Limitation Unit (TLU) as a function of airspeed in order to avoid excessive load transmission to the aircraft.

Three Flight Control Primary Computers (PRIM) which can process all three types of control laws (Normal, Alternate, Direct) The two sidestick controllers are not coupled mechanically, and they send separate sets of signals to the flight control computers. • Two Flight Control Secondary Computers (SEC) which can process the Direct Control Law. Two pairs of pedals, which are rigidly interconnected, give the pilots mechanical control of the rudder. The pilots control speedbrakes with a lever on the center pedestal.

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Airbus A340 Flight deck and systems briefing for pilots

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