From a report on the 915......
The initial climb rate was almost 2,000fpm at 70kt which (bearing in mind the density altitude) was pretty respectable, while at 7,000ft MSL the increase in performance really was very noticeable. The turbocharger worked as advertised, with no discernible reduction in manifold pressure, and having trimmed forward and set ‘max cruise’ of 5,500rpm and 37 inches of manifold pressure the IAS soon settled on 135kt for a TAS of 150 while burning 34-35 lit/hr.
Pretty impressive numbers, and although if you’re a long-term Rotax pilot you might be thinking that 35 lit/hr is quite thirsty, I’d counter that 150kt TAS is quite fast! Pull the power back a long way to say 4,800rpm and seventeen inches, and the engine is now just barely sipping litres per hour at 80kt TAS, while a good compromise (Bristell call it the ECO setting) of 5,000rpm and 36ins of manifold pressure still give a TAS of around 145kt at 7,000ft AMSL.