Rotax 912-UL User Manual

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page 2 - 2
Jan. 01/2007
Effectivity: 912 Serie
OM Edition 1 / Rev. 0
BRP-Rotax
P
Performance (ISA) (912 UL / A / F) 10 - 1
Performance (ISA) (912 ULS / S) 10 - 5
Performance data 10 - 4, 10 - 8
Performance graphs for stand. conditions
(ISA) 10 - 3, 10 - 7
power take-off side 7 - 3
Pre-flight checks 10 - 15
Propeller gearbox 9 - 5
Propeller governor 9 - 6
R
Remarks 3 - 1
Repeating symbols 4 - 1
Reporting 12 - 4
S
Safety 4 - 1
Safety information 4 - 2
Speed (912 UL / A / F) 10 - 1
Speed (912 ULS / S) 10 - 5
Symbols 4 - 1
T
Table of lubricants 10 - 12
Take-off 10 - 17
Technical data 8 - 1
Technical documentation 4 - 5
Throttle response 10 - 17
Trouble shooting 12 - 1
Type 7 - 2
Type description 7 - 2
V
Vacuum pump 9 - 6
W
Warming up period 10 - 17
Weights 8 - 1

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)