@Angus, if you take a look at RAE speed curves, most of them note the results are corrected to 95% takeoff weight. There are a few exceptions of course. I think they opted for an avarage, half fuel load value as standard.
5% takeoff weight diffo is quite a lot btw. For a mk9, it's around 370 lbs...that's quite a poop.
Or about half the weight of the internal fuel load. How much it would effect max speed depends on the altitude - more weight requires higher AoA in level flight, thus means more drag, the speed diffo is afaik 1-2%, ie. 4-8mph, and should be more noticable above rated altitude. but that's just a sidenote.
@1K3. I think our one has the low altitude AM engine. It makes sense since it's an important model, and the high alt ones are more-or-less represented by the 109K. BTW, there was a 3rd engine mounted in the G-14/AS versions, the 605 ASC, 2000 PS output, similiar to the 605DC of the 109K.