Rotax 914 series Maintenance 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 914 series Specifications

General

Bore	79.5 mm
Stroke	61 mm
Compression Ratio	9.0:1
Cooling System	Liquid-cooled cylinder heads, air-cooled cylinders
Redline	5800 rpm
Engine Type	4-cylinder, 4-stroke
Fuel Type	Avgas 100LL
Oil System	Dry sump
Fuel System	fuel injection
TBO (Time Between Overhauls)	2000 hours
Displacement	1.211 liters (1211 cc)
Power Output	84.6 kW (115 hp) at 5, 800 rpm