I see nobody has addressed these questions. So at flight speed yes the thrust (dynamic thrust) issue is much the same as the HP issue. There is no value in a static trust number for our airplanes. Every lift equation I know of use velocity. So if velocity is zero (static) the ship won't fly. You need to keep your eye on the concept of pitch speed.
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Good to see there is at least one other person who realizes how unimportant static thrust is. If static thrust was so important we'd all be flying with helicopter rotors bolted to the nose of our aircraft. Dynamic thrust potential depends on power and efficiency of the propellor system.