1) They explicitly said TVC is coming and that is not a question.
2) The discussion about how the J-20's mission profile requires an assumption of operating in unsupported situations was in the context of how CAC built a lot of system redundancies into the airframe, in fact *too many redundancies*, and how subsequent production batches, in consultation with operator feedback, have refined exactly what kinds of redundancies should be deprecated or added in, or else improved on the efficiency of those redundancies.
3) They explained the reason TVC isn't being tested on this current airframe is because the thrust increase itself is such a gain in capability they want to test what the plane can do with the new engine first before figuring out exactly what kinds of optimizations and requirements they want with TVC.
4) They *never* said systems redundancies were more important than TVC. The systems redundanchy conversation and the TVC were two completely seperate threads of discussion.
5) They *never* mentioned TVC only coming once subsystems became lighter weight or after a higher thrust variant of the WS-15.
6) They didn't say anything about system redundancy causing difficult maintenance. The "difficulty" was that it made production less efficient.