No, the third stage is essential if you want to get 70t to LEO. Otherwise, you wouldn't reach the delta V for orbit.
But why will it not have the delta V for orbit?
Falcon Heavy, with lower total thrust in its first and second stages and lower specific impulse, than the equivalent stages of CZ-5DY, is capable of launching 63.8t to LEO.
For the three core CZ-5DY, with its central core first stage having larger fuel tanks (and presumably longer burn time) than the single core version, and the second stage having two YF-100s rather than one, that all seems like a very plausible configuration for a 70t to LEO configuration.
A three stage to LEO rocket would be quite the exception around the world, would it not?