Rotax 912 i series - Technical Data; Fuel Consumption; Direction of Rotation

Effectivity: 912 i Series BRP-Powertrain page 1-14
OM Edition 1/Rev. 2 April 01/2014
d05694.fm
1.9) Technical data
See table
1.10) Fuel consumption
NOTE: This table is valid only for engine operation without
faults. In case of faults a higher fuel consumption
may occur.
See table
1.11) Direction of rotation
Direction of rota-
tion on propeller
shaft
Direction of rotation on propeller shaft: counter clockwise, looking
at p.t.o side of engine.
Fig. 4
Description 912 iSc/iS
Bore 84 mm (3.31 in)
Stroke 61 mm (2.40 in)
Displacement 1352 cm
3
(82.5 in
3
)
Compression ratio. 10.8:1
Fuel consumption in l/h
(US gal/h)
912 iSc/iS
At take-off performance (5800 rpm) 26.1 l/h (6.9 gal/h)
At max. continuous performance (5500 rpm) 23.6 l/h (6.2 gal/h)
At 75 % continuous performance 16.5 l/h (4.3 gal/h)
Specific consumption at 75 % continuous per-
formance
250 g/kWh (0.41 lb/
hph)
normal direction of propeller rotation (engine)