What activates the air bleed thermal anti-icing system under normal circumstances?

The definition of icing conditions on Embraer 145 & 135 is:

Bleed air for the engine inlet ice protection system comes from:

EICAS “E1(2) A/ICE FAIL” caution will appear for low and high pressure in delivery line, initiated by:

Where does the air leaving the horizontal stabiliser anti ice system leave the aircraft ?

Under and over pressure, and what else will trigger a “FAIL” caution message of the bleed air systems?

The windshield heating system is designed to maintain screen temperature between:

Windshield heating monitoring will activate a “W/S 1(2) HEAT FAIL caution at:

How are the sensors controlled ?

In automatic mode the pitot and static heating is applied:

EICAS caution messages relating to heating sensor failure are:

What cockpit indications tell the pilots that the main anti ice system is working ?

EICAS (blue) advisory message “CROSS BLD OPEN” will show whenever:

If in flight you suspect icing conditions but the anti ice system has not triggered, you should:

The selection for the windshield wiper is by:

The maximum speed for use of wipers is:

If the thermal anti icing system is activated below 24,600 ft, what happens to air conditioning ?

To perform the full ice detection test on the ground:

With the override switch at the AUTO position, in flight, when will the thermal anti ice activate ?

How do the ice detectors work ?

If the windshields overheat, resulting in an EICAN caution W/S 1(2) FAIL:

What are the cycle options of the windshield wipers ?

Which side of the pneumatic system supplies the horizontal stabiliser sub-system ?

What will happen to the airframe (wings and stabilizer) anti icing system if switched on after landing?

To perform the full ice detection test on the ground:

What is the limit for testing ice detection system in flight ?

After an ice encounter, EICAS blue advisory message appears. How can it be cleared ?

When applying de-icing fluid on the aircraft tail:

When performing full anti ice system on the ground, how many times should the test be performed ?

During an ice encounter in flight, or anti ice test in flight, what happens to the bleed temperatures ?