Download Airbus A330 Flight deck and systems briefing for pilots by Airbus PDF

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A330 Flight deck and structures briefing for pilots [Loose Leaf Publication]..LOOSE LEAF UNBOUND variation NO BINDER.

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Three batteries nominal capacity 37 Ah, 28 V each : - Two batteries used : . in emergency configuration to feed some equipment during RAT deployment or when CSM/G not operating. On ground to provide an autonomous source. 2 A330 electrical system Distribution - normal configuration AC distribution network ELEC DC • In normal configuration, each engine-driven generator supplies its associated AC BUS. • The AC ESS BUS is normally supplied from AC BUS 1. DC BAT BAT 1 25 V 5A DC 1 DC APU BAT 2 26 V 0A DC ESS APU BAT 25 V 5A DC 2 STAT INV DC distribution network • In normal configuration, normal DC systems are split into two networks : DC BUS 1 in parallel with DC BAT BUS and DC BUS 2.

Regardless of pilot inputs, the computers will prevent : - excessive maneuvres - exceedance of the safe flight envelope. 3 A330 flight controls - EFCS Computers Electrical control of the main surfaces is achieved by two types of computers : • three flight control primary computers (PRIM) which can process all three types of control laws (Normal, Alternate, Direct) • two flight control secondary computers (SEC) which can process the Direct Control Law. These computers perform additional functions including : • speebrakes and ground spoiler command • characteristic speed computation (PRIM only).

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. This function is achieved by the secondary computers. The rudder trim controls the rudder pedal zero load position as a function of pilot manual command on a switch located on the pedestal (artificial feel neutral variation). This function is achieved by the secondary computers. Yaw damper commands are computed by the primary or secondary computers In case of total loss of electrical power or total loss of flight controls computers the back up yaw damper unit (BYDU) becomes active for yaw damping function.

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