Usually it means showing an alarm, putting the system relying on it on degraded mode and letting the pilot manually select the sensor he thinks is correct.
Reacting to such failures is a big part of an equipment certification process.
In designing airframes, there's actually guidance along these lines to remove the ambiguity of how many sensors are necessary. You can use calculations to define what level of reliability is sufficient. As an example to this point, there are standards like IEC 61508 that outline the procedure for doing such calculations. Many organizations also create their own standards (e.g., five redundant sensors for mission critical systems, self-diagnostic sensors for safety critical systems etc.) It shouldn't be guesswork. It's a risk-based decision, not a subjective guess as to whether two or "a hundred" sensors are necessary.
No, no, no. This is just more of shifting the blame from Boeing upper management. They couldn't use two Angle of Attack (AOA) sensors as when there was a differing reading there would be no way to know the correct reading, which is why MCAS used a single AOA sensor on the right-hand side.