914 manifold pressure?
I’ve seen documented by Rotax that the 914 is able to maintain 115 HP up to 8,000 FT pressure altitude and a 100 HP up to 16,000 FT pressure altitude.
After having flown behind one for a quite a few hours at various altitudes in Idaho, I’m noticing I can only get 40” of manifold around 3,000 FT MSL. At 4,800 FT MSL it drops off to about 38” of manifold. At 6,500 FT MSL I was only getting 34.5”.
Shouldn’t you see 40” of manifold at 100% throttle setting (115 HP) at 6,500 FT MSL? Could airbox temperature be limiting this? Thanks!