A 70% battery mass fraction seems like a huge engineering challenge for an aircraft. I did a quick calculation of fuel mass fraction for the various Boeing 777 models [0] which ranged from ~13% to ~36%.
I don't see that the engineering is hard. You could just take an existing design and replace most of the cabin with batteries.
Building an economically viable mass-market aircraft with a 70% mass fraction might be another question, but if we're just talking about the engineering challenge of building it at all I don't think that's hard?
And on top of that, "refueling" wouldn't cost the 250k figure that usually gets thrown in comments.
I imagine it being more in the space of a 1-2k$ ; in which case the reduced passenger capacity might still be worth the premium in batteries.
Not saying it's impossible. Just hard.
[0] https://en.wikipedia.org/wiki/Boeing_777#Specifications