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Either way, anti-ice does use a lot more fuel.
You'll want to use engine anti-ice when flying through visible moisture when the TAT is below 10C or in icing conditions (i.e. snow, freezing rain etc.). Engine anti-ice should be turned off below -40C SAT.
Wing anti-ice uses a LOT of hot bleed air, and is best referred to as a de-icer, i.e. you wait for a build-up of ice first. Once you can visibly see ice on the wings, on the cockpit windshield, on certain probes or through computers telling you there's an ice build-up (none of which are simulated correctly in X-Plane yet), you would then want to switch on the anti-ice for a few seconds to shed the ice, then turn it off. Wing anti-ice in action
You want to prevent ice build up on the engine leading edges, but it's not so much of a problem on wings until you have lots of ice, particularly towards the wing tips where the airfoil is thinner.
Zibo 738 already has icing, however lack of visual icing cues that real pilots use is pretty bad.
Engine icing protection is used as anti-ice, but the wing icing protection is only used as a de-ice (since the ice could melt on the leading edge, but then re-freeze on the top and bottom of the wing as a smooth almost invisible ice that is impossible to remove in-flight).
Also turning on wing anti-ice should set the FMC into a special icing mode until the end of the flight, but I don't think it's simulated in zibo (definitely not in the default 738).
Seasons would be a nice touch tho. It’s okay considering it’s summer rn but winter is coming :(
Positioning the WING ANTI–ICE switch to ON in flight:
• opens both control valves
• sets stall warning logic for icing conditions.
Note: Stall warning logic adjusts stick shaker and minimum maneuver speed
bars on airspeed indications. FMC displayed VREF is not adjusted
automatically.
Note: Stall warning logic remains set for icing conditions for the remainder
of the flight, regardless of subsequent WING ANTI–ICE switch
position.
[Option]
An advisory only ice detection system detects airplane icing in flight. The system
consists of a probe located on the forward left fuselage and advisory lights located
on the left forward panel.
When the probe senses ice build–up inflight, the ICING light illuminates. When
ice has previously been detected and the probe is no longer detecting ice, the
ICING light will extinguish and the NO ICE light will illuminate. The ICING light
and the NO ICE light do not illuminate simultaneously.
Note: Residual ice may remain on the window areas with the NO ICE light
illuminated.
The ICE DETECTOR light, located on the forward overhead panel, will
illuminate if the ice detection system fails. Illumination of the ICE DETECTOR
light also illuminates the MASTER CAUTION and ANTI–ICE system
annunciator lights.
The hard part would probably be realistic ice detection and its display as an ICING light or as a windshield "texture".