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Additional info for Airbus A340 Flight deck and systems briefing for pilots
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. • Each DC network is supplied by its own TR. • More specifically, ESS TR systematically feeds DC ESS BUS, which allows a better segregation between DC 1 and DC 2. • Two batteries are connected to the DC BAT BUS via the Battery Charge Limiter (BCL). • Each battery has its own HOT BUS bar (engine/APU fire squib, ADIRS, CIDS, PRIM and SEC computers, slide warnings, parking brake, etc).
APU TR …………………………………. SWTG FUEL BUS …………………….. AUDIO ACP CAPT …………………….. AIR BLEED VLV ENG2 ……………….. XFEED VLV ENG1 MOT1-2 ………….. 6 4. 2 A340 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 back-up. 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.
These two FCDCs ensure the electrical isolation of the flight control computers from the other systems. 4 A340 Flight Controls - EFCS Power sources Electrical power supply The flight control computers PRIM, SEC and FCDC 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 A340 Flight Controls - EFCS Power sources Hydraulic power supply Three hydraulic circuits (Green, Yellow, Blue) power the flight controls.