Rotax 915 i A SERIES - Page 27

Effectivity: 915 i A Series
Edition 0 / Rev. 0
BRP-Rotax Page 2-3
December 01 2017
Parameter Min. Max.
Operating Altitude
–
23000 ft
The engine performance is approximately proportional to the air
flow value.
The air flow information is available on the Display CAN Bus.
Acceleration
Limit of engine operation at zero gravity and in negative “g“
condition.
Parameter Min. Max.
Acceleration -0.5 g (max. 5
seconds
Static roll angle
The dry sump lubrication system warrants lubrication in every
flight situation
Parameter Min. Max.
Static roll angle ß 40°
Manifold
temperature
Parameter Min. Max.
Manifold temperature 50 °C (120 °F)
Manifold pressure
Parameter Min. Max.
Manifold pressure 60 hPa
(1.77 in. HG)
1730 hPa
(51 in. HG)
Boost pressure
Parameter Min. Max.
Boost pressure ambient pressure 1730 hPa
(51 in. HG)