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When ECAM shows "ELEC ECMU 1 FAULT":

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According to this ECAM ELEC DC page:

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This ECAM ELEC page shows:

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As shown on this ECAM ELEC page, which BUS is normally supplying the ESS TR?

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What is the meaning of this ECAM?

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The MAINT BUS switch is located:

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With APU GEN and external powers supplying the network:

Correct! Wrong!

An engine generator is driven:

Correct! Wrong!

What is the meaning of this ECAM?

Correct! Wrong!

During EMER GEN automatic start up sequence:

Correct! Wrong!

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According to these indications:

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The APU battery:

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On C/B ECAM page, the pilot reads "NORMAL". What does it mean?

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According to this ECAM ELEC page:

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One function of the Electrical Contactor Management Units (ECMU) is:

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Correct! Wrong!

The Emergency generator is powered by:

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The minimum number of generators required to supply the whole network is:

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Loss of one generator or TR (except, if lost is due to over current detection) provides:

Correct! Wrong!

When the MAINT BUS switch is on:

Correct! Wrong!

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The EMER GEN is powered by a hydraulic system pressurized by an engine driven hydraulic pump. Pressing the LAND RECOVERY p/b switch will:

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According to these indications which AC BUS supplies the ESS TR?

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In flight, APU not running, an engine generator has failed. What is supplying the corresponding AC BUS?

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What is the meaning of this ECAM?

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According to this ECAM ELEC page:

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The main function of the MAINT BUS switch is:

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Each engine generator supplies power to:

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Two Electrical Contactor Management Units (ECMU) provide:

Correct! Wrong!

Airbus A340 - Electrical Power