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Additional info for Airbus A319, A320, A321 Flight deck and systems briefing for pilots
Z AC ESS BUS is normally supplied from AC BUS via a contactor. z DC BAT BUS and the DC ESS BUS are normally powered by the TR 1. z Two batteries are connected to the DC BAT BUS via the Battery Charge Limiter (BCL). z Each battery has its own HOT BUS bar (engine / APU firesquib, ADIRS, CIDS, ELAC 1, SEC 1, slide warnings, parking brake etc). 6 A319/A320/A321 normal electrical flight configuration z In case of failure, the failed generator is automatically replaced by : - the APU generator if available - the other main generator with automatic partial galley load shedding.
As basic flight mode : z Coordinated roll and yaw surfaces deflections : - to achieve and maintain bank angle up to 33°, stick released z Bank angle protection above 33° : - positive spiral stability restored up to 67° inside normal flight envelope - limit of 67° bank angle z Lateral control laws providing handling quality features such as : z Engine failure or aircraft asymmetry compensation consisting of : - If no pilot action : • stabilized sideslip and bank angle followed by, • automatic rudder trimming to compensate asymmetric thrust • slowly diverging heading.
Recommanded action : • zero sideslip target with pedals (take-offf, goaround), • heading stabilization with stick input, • steady flight stick free / no pedal forces (rudder trim). z Adaptation of basic control law objectives to : - bank angle resistance to disturbance, stick free, precise piloting good turn coordination, dutch roll damping, sideslip minimization. z Sidestick free with pedal deflection results in stabilized sideslip and bank angle facilitating “de-crabbing” in crosswind landings.
Airbus A319, A320, A321 Flight deck and systems briefing for pilots