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

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

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Circuit-breakers are monitored by the CBMU (CircuitBreaker Monitoring Units) which output the identification and status of each circuit-breaker. • A specific C/B page is provided on the ECAM. • Computer resets can be performed via system controls. 755/92 Issue 4 C/B ECMU1 VOLT SNSG …………………. SFCC1 NORM DCBUS AVAI ………... HYD PUMP G ENG2 …………………. ANTI ICE ENG2 ……………………….. DU SWTG CAPT ND …………………. HYD PUMP B ENG1 ………………….. ADIRU1 155VAC ……………………… ANTI ICE PITOT 1 OR 3 …………….. 303PP …………………………………..

4 A330 flight controls - EFCS Power sources Electrical power supply The flight control computers (primary, secondary and Flight Control Data Concentrator) are fed by various DC busbars. This ensures that at least two flight control computers are powered in the event of major electrical power losses such as - failure of two main systems or - electrical emergency configuration (CSM-G) or - battery-only supply. 5 A330 flight controls - EFCS Power sources Hydraulic power supply Three hydraulic circuits (Green, Yellow, Blue) power the flight controls.

755/92 Issue 4 C/B ECMU1 VOLT SNSG …………………. SFCC1 NORM DCBUS AVAI ………... HYD PUMP G ENG2 …………………. ANTI ICE ENG2 ……………………….. 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).

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