Earlier quoted context omitted.
Well, if the primary is known not to be in a good state, you might as well fail over and hope that the issue was a fried disk or a cosmic bit flip or something. The real safety feature is the 4 hour lead time before manual processing becomes necessary. One of the key safety controls in aviation is “if this breaks for any reason, what do we do”, not so much “how do we stop this breaking in the first place”.
I'm no aviation safety controls expert but it seems to me that there are two types of controls that should be in place: 1. Process controls: What do we do when this breaks for any reason. 2. Engineering controls: What can we do to keep this from breaking in the first place? Both of them seem to be somewhat essential for a truly safe system.
https://en.m.wikipedia.org/wiki/Hierarchy_of_hazard_controls