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

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One of the three PRIM is selected to be the master ; it processes the orders and outputs them to the other computers PRIM 1, 2 and 3, SEC 1 and 2) which will then execute them on their related servo-loop. • The master checks that its orders are fulfilled by comparing them with feedback received ; this allows self-monitoring of the master which can detect a malfunction and cascade control to the next computer. The two secondary computers (SEC) : • are able to process direct laws only • either SEC can be the master in case of loss of all primary computers • each SEC can control up to 10 servo-loops simultaneously ; each can provide complete aircraft control.

DU SWTG CAPT ND …………………. HYD PUMP B ENG1 ………………….. 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 A330 hydraulic system General • Three fully independent systems : Green, Blue, Yellow (nominal pressure at 3000 psi). • Normal operation : - four engine-driven pumps, two of which are for the Green system - three electrical pumps that can act automatically as backup They are managed by the HSMU (Hydraulic System Monitoring Unit) which ensures all autofunctions (electrical pumps, RAT, monitoring, etc) ; manual override is available on the overhead panel.

According to number and nature of subsequent failures, it automatically reverts to : - Alternate Law, or Overall Normal LAW schematic - Direct Law.

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