Oddly enough, the later models of the A-20 (H & J) were capable of speeds up 351 mph, just 4 mph less than the A-26. Our version should be able to pull close to 330 mph at optimal altitude of 14,000 feet. Those later models had another 400 hp on tap.
It should be noted that the A-26, as used in WWII carried no more ordnance than the A-20G. Later modifications upped that to over 8,000 lbs.
Another oddity of the A-26 was the effect its laminar flow wing had on takeoff. You didn't rotate the A-26. If you tried, it just mushed, refusing to lift. Pilots simply let the plane fly itself off the runway. Once airborne and safely above minimum single-engine speed, it climbed very well for its size. Handling was very similar, with most pilots giving the nod to the A-26 as being more maneuverable, largely due to its greater reserve of power. Turn radius was about the same.
My regards,
Widewing