BRP ROTAX 916 i A Series User Manual

Effectivity: 916 i A / C24
Edition 0 / Rev. 1
BRP-Rotax Page 2-3
December 01 2023
NOTE
From 20000 ft. up to 23000 ft. altitude a warning lamp may
flash. Operating the aircraft in this altitude range presents no
danger to the operator and does not limit the function of the
engine.
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
(Note*)
–
50 °C (122 °F)
Extended Manifold
temperature (Note**)
> 50 °C (122 °F) 80 °C (176 °F)
Note* rated power performance is provided
Note** reduced power performance as provided in section
“Extended Manifold Temperature Range – Power Performance
Impact”
Extended Manifold
temperature range
Power Performance Impact
Power Performance Continuous
Performance
Take-Off
Performance
Resulting Power
reduction
- 1 kW - 2.7 kW

BRP ROTAX 916 i A Series Specifications

General

Brand	BRP
Model	ROTAX 916 i A Series
Category	Engine
Language	English