My apologies, you are correct.
Adding the figures above to the original kpp acceleration requirements gives the following transonic acceleration times from M0.8 to M1.2 at 35K:
F-35A: 63 seconds.
F-35B: 81 seconds.
F-35C: 118 seconds.
The source of the above does note that that the A and B figures above beat all configurations of the F-16, and the C about half.
I’d post a link but it has a bl*gspot in the URL.
Which does remind me the F-35 was designed as a bomb truck with essentially the same dynamic performance as the F16 as a cheap to operate replacement. Accepting that it is rarely expected ever to go supersonic, I can see where limiting the envelope is a cost effective saving.
Dubious about the explanation for not addressing the hydraulic system issue though. It hasn’t blown a tyre in the wheel bay so far so we don't have to worry about it?