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Extra resources for Airbus A319, A320, A321 Flight deck and systems briefing for pilots

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Green/Yellow system may be pressurized by the PTU. z Abnormal operation : - if engine No. 1 inoperative or Green pump failed : then Green system pressurized by the reversible Power Transfer Unit (PTU) - if engine No. 2 inoperative or Yellow pump failed : then Yellow system pressurized by the reversible PTU - if Yellow system pump inoperative and PTU failed : then an electric pump will pressurize the Yellow system. - if case of dual engine failure or total electrical power loss : the Ram Air Turbine (RAT) will pressurize the Blue system.

Z Sidestick free with pedal deflection results in stabilized sideslip and bank angle facilitating “de-crabbing” in crosswind landings. 5 second after lift-off or touchdown. 14 A319/A320/A321 alternate law z Flight mode as basic control laws : - pitch axis : as normal law, stick deflection to change Nz, - roll/yaw axes : direct stick-to-roll-surface relationship, speed, configuration and surface availability dependent, - automatic pitch trim. z Loss of flight envelope protections except : - manoeuvre protection against excessive load factor - low speed stability - conventional aural stall and overspeed warning z Reversion of basic control law : - alternate law not being adapted to landing phase automatic reversion to direct law after landing gear extension.

Amber message on PFD (“USE MAN PITCH TRIM”) z Loss of all flight envelope protections : z Manual trimming through trim wheel : - red message on PFD (“MAN PITCH TRIM ONLY”) - conventional aural stall and overspeed warning. z Automatic reconfiguration after loss of basic control law in either axis. 16 Performance comparison of sidestick/FBW and conventional controls z A300 flying testbed equipped with dual sidestick/FBW system (left side) and control column conventional flight control system (right side).

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