Years back the speculation was that WS-10 had poor throttle response time, relevant for carrier landing scenarios that involve transitioning from low throttle approach to max throttle on touchdown so that, in the event that the aircraft misses all arrestor wires, it can subsequently recover and go around rather than running off the deck and into the sea. Perhaps this shortfall has yet to be resolved.
That was originally from like over a decade ago now. I'm not sure if it has any relevance to the last couple of years.
It is interesting to contemplate what other technical characteristics might impinge on suitability for carrier applications but be of lesser importance for land-based applications. Resistant to saltwater corrosion? Stability and granularity of response at low throttle settings? Resistance to foreign object damage and associated ease of maintainability and repair given limited onboard facilities? Mechanical durability characteristics associated with high dynamic loads experienced in both catapult take-off and arrested recovery?
From memory, about a year ago the usual trio/grapevine said that WS-10 was satisfactory for implementation aboard the J-15 family, but one of the reasons for continuing to buy Al-31s was to support the Russian aerospace sector, helping Saturn out.
Of course, whether one believes that is another matter, but their track record is what matters.
How the PLAN will go with J-15 family engines in future, who knows.

