F
Rotax’s words specific to that engine.
Power loss relative changes in elevation aren’t fixed across different engines, and on a system that’s compounded by a turbo, it gets even more complicated than a linear percentage loss.
Case in point - does a 5hp engine stop making power past 1k feet elevation?
The question was asked and Skank posted his results. The guy does a lot of testing and has real world experience with these tunes at that elevation.
Fack
Power loss relative changes in elevation aren’t fixed across different engines, and on a system that’s compounded by a turbo, it gets even more complicated than a linear percentage loss.
Case in point - does a 5hp engine stop making power past 1k feet elevation?
The question was asked and Skank posted his results. The guy does a lot of testing and has real world experience with these tunes at that elevation.
Fack
A chart in a Rotax Aircraft Engine Shop manual says 5hp loss for every 1000ft elevation increase. [Lazair Aircraft w/503 fan manual]
Ok then, according to BRP values, then...
@ sea level, 165hp
@ 8000 ft, 165hp
@ 9000 ft, 160hp
@ 10000 ft, 155hp
@ 11000 ft, 150hp
@ 12000 ft, 145hp
Since its a constant, then...
Stage 3, 95 octane is 30+hp
@ sea level, 195hp
@ 8000 ft, 195hp
@ 9000 ft, 190hp
@ 10000 ft, 185hp
@ 11000 ft, 180hp
@ 12000 ft, 175hp
...so what if it lost power? I'd still be happy with that at 12k feet.