Rotax 912 Series Service Manual

Effectivity 912/914 Series
Edition 1 / Rev. 0
page 61
May 01/2007
d02623
73-00-00
BRP-Rotax
Maintenance Manual
3.8) Connecting fuel lines (tank)
The fuel lines from the tank to the fuel pump, from the fuel pump to the two
carburetors and the return line to the fuel tank must be installed as per the
aircraft manufacturer’s instructions when installing the engine in the aircraft.
■ CAUTION: When tightening the fuel lines, no force or torque may be applied
to the fuel pump connections or the fuel pressure regulator.

Rotax 912 Series Specifications

General

Redline	5800 rpm
TBO	2000 hours
Displacement	1211 cc
Bore	79.5 mm
Stroke	61 mm
Power Output	80 hp (59.6 kW)
Compression Ratio	9.0:1
Fuel Type	Avgas 100LL
Ignition System	Dual electronic ignition
Fuel System	Fuel Injected
Oil System	Dry sump
Engine Type	4-cylinder, horizontally opposed, 4-stroke