…weren’t as bad as originally reported. I found this interesting, though:

As for the engine shutdown issue, data analysis has yet to result in any definitive conclusions. Although the analysis will continue, the observation that this particular engine had undergone a comparatively high degree of pre-flight testing, may ultimately lead to the conclusion that the shut down was related to the accumulating fatigue of an engine firing more than its nominal mission requirements. If this turns out to be the case; it would prove to be both somewhat ironic, as well as easily addressed by limiting cumulative firings for flight engines. Ongoing analysis has likely pushed the likely date of the next Dragon flight to ISS into the early March time frame.

Wouldn’t “limiting cumulative firings for flight engines” have interesting and problematic implications for reusability?

If this is really a problem, sounds like they’ll have to have a more robust engine design (or perhaps downgrade performance) for reusable versions. And of course, it’s possible that the new engine to start being used next year will resolve whatever the issue is.