Rotax 912 i series Operator's Manual

Effectivity: 912 i Series BRP-Powertrain page 4-2
OM Edition 1/Rev. 1 July 01/2012
d05873.fm
4.1) Fault indicated by the EMS lamps
EMS lamps
The aircraft should be flown to the nearest available landing site
(Airfield, Airstrip, Airport) if any of the following combinations of
the EMS lamps arise:
- One lamp permanently on, one off.
- One lamp permanently on, one flashing.
- Both lamps permanently on.
- Both lamps flashing.
EMS lamps operat-
ing states
If one of the lamps is flashing while the other is off then limited
flight operation are permitted up to a maximum of 10 hours.
ON = permanently on

WARNUNG
NOTICE
Reduce engine power setting to the minimum
necessary and curry out precautionary land-
ing.
LANE A LANE B Action
OFF Flashing Limited flight operation
Flashing OFF Limited flight operation
OFF ON Land the aircraft
Flashing Flashing Land the aircraft
Flashing ON Land the aircraft
ON OFF Land the aircraft
ON Flashing Land the aircraft
ON ON Land the aircraft

Rotax 912 i series Specifications

General

Number of Cylinders	4
Max Power	100 hp (73.5 kW)
Max Power Output RPM	5800 rpm
Ignition System	Dual electronic ignition
Oil System	Dry sump, forced lubrication with separate oil tank
Reduction Gear Ratio	2.43:1
TBO	2000 hours
Engine Type	4-stroke, horizontally opposed
Displacement	1352 cm³
Bore x Stroke	84 mm x 61 mm
Max Torque	128 Nm
Fuel Type	Avgas 100LL or unleaded automotive gasoline
Fuel System	Electronic fuel injection
Cooling System	Liquid/air-cooled