Generally, single crystal blades are designed for their resistance to creep at high temperatures. If your predominate creep mechanism is sliding at grain boundaries in a polycrystalline material, you can impart creep resistance by removing the grain boundaries. A single crystal is the limiting case of this process.
3D printed parts, so far, are polycrystalline, and would be used in other places in an engine's hot stage.
Happy to address specifics.
The dominant concerns I am aware of are low thermal conductivity, thermal stability, and lack of chemical attack in the environments in question.
There's a lot of buzz in the materials community around additive, but I think 3D-printed turbine blades are basically just a dream right now. People are still wrestling with getting consistent build quality for simple structural components...
I'd love to hear about this from a Metallurgical Engineer or a Material Science Expert.
[1] http://qz.com/667477/ge-fires-up-worlds-largest-commercial-j...