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ANTI ICE ENG2 ……………………….. DU SWTG CAPT ND …………………. HYD PUMP B ENG2 ………………….. ADIRU1 155VAC ……………………… ANTI ICE PITOT 1 OR 3 …………….. 303PP ………………………………….. BUS 1/3 TIE CNTOR …………………. ANTI ICE 1 OR 3 PHC ……………….. EXTRACT FAN AVNCS ………………. ADIRU1 AOA1 26VAC ……………….. APU TR …………………………………. SWTG FUEL BUS …………………….. AUDIO ACP CAPT …………………….. AIR BLEED VLV ENG2 ……………….. XFEED VLV ENG1 MOT1-2 ………….. 6 4. 2 A340 Hydraulic System General • Three fully independent systems : Green, Blue, Yellow (nominal pressure at 3000 psi).

The computers prevent from : - Excessive maneuvers - Exceedance of the safe flight envelope. 3 A340 Flight Controls - EFCS Computers Cockpit controls Electrical control of the main surfaces is achieved by two types of computers : Each pilot has a sidestick controller to exercise control of pitch and roll. • 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.

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.

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