AIR ENG 1+2 BLEED LO TEMP

TASK 36-11-00-810-886-A Low Bleed Temperature of the Engine 1 in Climb

TASK 36-11-00-810-887-A Low Bleed Temperature of the Engine 1 in Cruise

TASK 36-11-00-810-888-A Low Bleed Temperature of the Engine 1 in Descent

TASK 36-11-00-810-893-A Low Bleed Temperature of the Engine 2 in Climb

TASK 36-11-00-810-894-A Low Bleed Temperature of the Engine 2 in Cruise

TASK 36-11-00-810-895-A Low Bleed Temperature of the Engine 2 in Descent

For details see TSM effectivity for your A/C

— RESET PROCEDURE—

36-11-00-740-001-A BITE Test of the BMC 1(2)

MMEL 36-11-04 Engine Bleed Fan Air Valve

36-11-34 PB 401 BLEED MONITORING COMPUTER (BMC) replace

Read me first

All instructions and limitations given in those documents that relate to the resetting of systems both on the ground and in the air must be respected. No reset should be attempted without a thorough appreciation of the technical ramifications. No more than one computer should be reset at any one time. No reset should be attempted in flight unless specifically permitted by the QRH. Maintenance messages remaining after a reset require engineering investigation.

If you encounter an ECAM warning or caution that is not available on our website, please take a photo and send it to our Telegram.

Likewise, if you detect any discrepancies on the site, you can report them directly in our Telegram.

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