Rotax 912-UL User Manual

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page 12 - 4
Jan. 01/2007
Effectivity: 912 Serie
OM Edition 1 / Rev. 0
BRP-Rotax
12.1) Reporting
According to the regulation of JAR / FAR 21.3 the manfacturer shall evaluate
field information and report to the authority.In case of any relevant occur-
rences that may involve malfunction of the engine, the form on the next page
should be filled out and sent to the responsible authorized ROTAX distributor.
◆ NOTE: The form is also available from the official ROTAX AIR-
CRAFT ENGINES Homepage
www.rotax-aircraft-engines.com
in electronic version.

Rotax 912-UL Specifications

General

Displacement	1211 cc
Bore x Stroke	79.5 mm x 61 mm
Compression Ratio	9.0:1
TBO (Time Between Overhaul)	2000 hours
Engine Type	4-cylinder, 4-stroke
Power Output	80 hp
Cooling System	Liquid/air-cooled
Fuel Type	Avgas 100LL or unleaded automotive gasoline
Oil Capacity	3 liters
Fuel System	2 carburetors
Oil System	Dry sump forced lubrication with separate oil tank
Reduction Gear Ratio	2.43:1
Max Continuous Power	75 hp (56 kW)