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Air is supplied to the aircraft’s pneumatic system via two HP ground connectors. The crossbleed valve has to be opened manually to provide air for both sides.

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The pneumatic system supplies high pressure air:

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Each pneumatic system is controlled and monitored by two Bleed Monitoring Computer (BMC) channels.

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Each system is controlled and monitored by one Bleed Monitoring Computer (BMC) channel.

If an engine bleed pylon leak is detected, both bleed valves on same side will close, the X-Bleed Valve will receive a closure signal, and:

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A leak detection system is provided to detect and locate any overheat in the vicinity of the hot air ducts.

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With an APU leak signal:

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Air is normally bled from the intermediate pressure stage (IP) of engine HP compressor, to minimize fuel penalty.

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The LH and RH bleed valves are pneumatically-controlled by BMC1 and BMC2 respectively, and are electrically-operated.

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The LH and RH bleed valves are electrically-controlled by BMC1 and BMC2 respectively, and are pneumatically-operated.

High pressure air is supplied from:

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With APU supplying the pneumatic system and X-Bleed Valve set on Close position:

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Each pneumatic system is designed to:

Please select 2 correct answers

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Airbus A340 – Pneumatic System