Based on my reading of FAR 25, specifically 25.143 - 25.207, I can't agree it's possible for a transport category airplane to be unstable. So I guess I don't kn

Based on my reading of FAR 25, specifically 25.143 - 25.207, I can't agree it's possible for a transport category airplane to be unstable. So I guess I don't know what you mean by "inherent instability". I also am unconvinced computers can mediate an airplanes aerodynamic design in order to achieve certification under this part, because again by my reading the expectation is that we (pilots and the flying public) can expect static and dynamic stability dynamic stability, laterally and longitudinally. Can computer control improve these behaviors? Sure. Can computer control make them more linear or consistent or docile or predictable? All of those things. But is it acceptable to have negative static stability, naturally occurring by design, in transport category aircraft moderated by computer? I don't think that's allowed but then I'm not deep diving these regulations either. What happens if all computer control goes down? You can't fall back on the natural static and dynamic stability of the airplane, because it doesn't exhibit those characteristics? That seems bad and not consistent with FAR 25. However, if any such computer safeguards can be disabled (either by the computer itself becoming confused and removing those safeguards; or by pilots disabling them explicitly), I expect the pilot to be trained as part of the type certification requirements, how the airplane behaves when the safeguards are enabled and disabled. I'm quite sure Boeing knows the answer to these questions. I suspect the FAA knows the answer to these questions. And when you say "we don't know" I think you mean HNer's engaged in discussion, who maybe aren't even aware that quite a lot of things are mandatory for obtaining transport category aircraft airworthiness certification.