In a non FIKI certified airplane, ice will not be an instant killer and you will often have some sort of ice protection system on larger airplanes, but that system is enough to get you out of icing conditions safely and not enough to permit you to continuously fly in icing conditions.
On a FIKI certified airplane, systems are in place to protect you from ice, but those systems have limits, and they use electricity/bleed air which means they use fuel which means that you should avoid known icing conditions whenever possible. And I don't believe anyone heats the trailing edges, actuators are strong enough to break off any ice that might form, and airflow is usually already turbulent enough by the time it reaches the trailing edges that ice probably wouldn't make any difference.
As to the answer to your question, I'll use the term surfaces loosely to refer to all areas that are heated:
We'll start with the 2 lighted icing indicators that are located under the windshield in full view of the pilots, 2 icing probes located on the underside of the cockpit, probes and ports of the pitot-static system, slats 3, 4, and 5 on each wing, air intake lip on both engine nacelles, both windshields, both forward and both aft lateral windows, and various components of the potable and waste water system that I am currently too lazy to list.
And yes, maybe the question would be better suited to someone who doesn't have the A-350 Technical training manual laying around the hard drive