From "The Focke Wulf Ta 152" by Hitchcock:
"Steel had long been planned for both the Fw 190 and the Ta 152; specifically for use in the wing spars and skinning despite a 15 to 25 percent weight penalty. "
Since the paragraph it is taken from is a discussion of the wing design I presume it is 15 to 25 percent of the total wing weight, not the entire aircraft.
250 kg would equate to a wing weight of 1000 to 1700 kg. I can't find any info on the wing weights but it doesn't seem reasonable to me.
"Focke Wulf Ta 152" by Dieter Harmann gives a breakdown of weights for the Ta 152 H-0 and H-1.