I calculated the wing loading WVL according to the Reynold's formulae, after I had found a scientific calculator , and I found that it is something above 11.
To be exact, 352 oz divided by 31.5 (9.98^1.5) = 11.17
It won't be a floater.
By the way I really wonder why no adv in the magazines mentions WVL, when indicating the wing loading of their products, even though it makes much more sense that the mere oz/sq.ft.