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4 A319/A320/A321 normal electrical flight configuration z In normal configuration, both normal AC systems are split z Each engine-driven generator supplies its associated AC BUS via its Generator Line Contactor (GLC). 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).

21 3. 2 A319/A320/A321 electrical system architecture The electrical power generation comprises : z Two engine-driven AC generators, nominal power 90kVA z One auxiliary power unit (APU) AC generator nominal power 90kVA z One emergency generator nominal power 5kVA, hydraulically driven by the Ram Air Turbine (RAT), automatically deployed in case of main generators loss z Two batteries, nominal capacity 23Ah each - on ground : to provide an autonomous source mainly for APU starting - in emergency configuration to feed some equipment : • during RAT deployment • after landing gear extension (only for A320).

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. z In case of total loss of all main generators, the RAT is automatically extended and drives the emergency generator via a hydraulic motor.

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


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