Originally Posted by
BUSSPilot
“Each engine has its own anti-ice system, with an independent hot bleed air source. The bleed air is extracted from the High Pressure Compressor to anti-ice the engine air inlet”
The above two sentences are an extract from the FCOM.
I suppose your doubt arises from the fact that wing anti ice is mentioned while, engine anti ice is not. As mentioned by the rest on this thread, it is independent - directly from the engine bleed to the engine nacelle.
Thank you! All good explanations.