Rotax 582 UL series Operator's Manual page 63

Index
A
Abbreviations ................................3
After engine start ...........................5
B
Before engine start.........................2
C
Cooling system ..............................2
Cylinder designation ....................15
D
Description of design....................12
Description of design 582 .............13
Dimensions .................................16
Direction of rotation ......................17
disposal ........................................1
E
Electric system ..............................5
Engine components .....................15
Engine preservation .......................2
Engine preservation — after
each flight....................................2
Engine preservation — at
engine stoppage of 1 to 4 weeks ...2
Engine preservation — at out of
service periods or storage of
engine for longer than 4 weeks
up to 1 year..................................2
Engine start ............................... 2–3
Engine views ...............................15
Exceeding cylinder head
temperature .................................2
Exceeding engine speed ................2
Effectivity: 582 UL
Edition 3 / Rev. 0
Exceeding exhaust gas
temperature .................................2
F
Fuel consumption ........................16
Fuel pressure ................................3
Fuel pressure too low .....................3
Fuel system...................................3
G
General.........................................2
L
List of effective pages.....................1
Lubrication system .........................3
O
Operating limits..............................1
Operating media Coolant................3
Operating media Fuel.....................4
Operating media Lubricants............6
Operation in flight...........................6
P
Performance data ..........................2
Pre-flight checks ............................2
Propeller gearbox ..........................6
R
Re-Start during flight ......................2
BRP-Rotax Page Index-1
January 01/2018