"So that leaves me wondering, okay why did Rotax only feel it necessary to publish this sort of a torque curve for the 914 and not for the 912?"
I am not completely sure of your question? because the 914 engine has two phases (struggling to find the good term for that): 100% continuous and 115% take off.
The 912 does not have this two-curve necessity as it is not turbocharged and has no "military power" throttle setting.
A constant speed prop is ideal for the 914 as you can utilize the best rpm and throttle position to get the best power, for both take-off and cruise.
A fixed pitch prop is always a compromise but on a STOL aircraft like the highlander you have so much drag a high cruise speed is not important so you can pitch for max climb with a long prop and be pretty darn happy.
Just don't pitch the 914 prop too heavy/coarse. Can you imagine the pressure/load on the pistons at only 4800rpm and 40inHG?? It was not designed for that. Fast moving pistons wear less as they have less transition/side load time and more rpm's give more power.