Rotax 912 Series Operator's Manual

Effectivity: 912 Serie
Edition 4 / Rev. 0
BRP-Rotax Page Index-1
November 01/2016
Index
A
Abbreviations ................................3
Abnormal operation........................1
After engine start ...........................8
Auxiliary equipment......................14
B
Before engine start.........................5
C
Cold weather operation ................10
Cooling system ..............................2
Cruising ........................................9
cylinder designation .....................17
D
Daily checks ..................................2
Direction of rotation......................19
E
Electric system ..............................6
Engine back to operation ................3
Engine components .....................17
Engine preservation and storage.....2
Engine shut-off ............................10
Engine start ............................... 5–6
Engine views ...............................17
Exceeding cylinder head
temperature .................................3
Exceeding engine speed ................3
Exceeding of max. admissible
coolant temperature .....................4
Exceeding of max. admissible
cooling system temperature ..........3
Exceeding oil temperature ..............4
F
Fire, Engine, compartment .............5
Form.............................................2
Fuel consumption ........................18
Fuel system...................................4
G
General.........................................2
L
List of effective pages.....................1
Lubrication system .........................5
O
Oil pressure...................................5
Oil pressure below minimum...........4
Oil pressure below minimum -
on ground ....................................5
Operating limits (912 A/F/UL)..........2
Operating limits(912 S/ULS) ...........5
Operating media Fuel.....................9
Operating media-Coolant ...............8
Operating media-Lubricants..........10
P
Performance data ..........................2
Pre-flight checks ............................5
Propeller gearbox ..........................7
R
Re-Start during flight ......................3

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