How much fuel weight will the current Crew Dragon carry? Will it be just enough for launch abort, or the full load (over 3000 lbs) needed for propulsive landing as a back-up to the parachutes?
I have seen different statements as to whether propulsive landing capability will be retained for parachute back-up.
The 3000 lbs estimate is from this answer about the early Dragon2. It was used for the pad abort test, but I'm almost certain this carried a full (propulsive) fuel load for thorough data collection.