There is more to gross weight limits than simple wing loading g limitations. A wing may be able to withstand 6 g’s at 1050 pounds without failure. However, your simple calculation doesn’t take into account the performance at weights greater than 1050. The power to weight loading may not be sufficient to allow for climb.
Simply put, you could yank on the stick and the wing won’t break. But the airplane is so heavy at 1432 pounds it can’t get above pattern altitude.
Short wings on a light aircraft can produce a speedy ship. But there’s always that pesky piper to pay.
Notice the heavy hauler gains a whopping 100 pounds in gross weight, but it takes six feet more wingspan to do it. The longer wings have a greater wing bending moment so the g limitation is lower. This tells me the Speedwing 1050 weight is near the limit of its performance. If you were to actually load the short wing to 1432 the induced drag may be so high it may not be possible to climb with just 100 hp.
John Pitkin
Greenville, TX