Rotax 912 Series Operator's Manual

4) Abnormal operation
Topics in this chapter
4.1 Re-Start during flight.............................................................................. 3
4.2 Exceeding max. admissible engine speed ................................................. 3
4.3 Temperature..........................................................................................3
4.3.1 Exceeding of max. admissible cooling system
temperature ................................................................................................ 3
4.3.2 Exceeding of max. admissible cyl. head
temperature ................................................................................................ 3
4.3.3 Exceeding of max. admissible coolant
temperature ................................................................................................ 4
4.3.4 Exceeding of max. admissible oil temperature .............................................4
4.4 Oil pressure/Fuel pressure...................................................................... 4
4.4.1 Oil pressure below minimum - on ground ................................................... 5
4.4.2 Oil pressure above permitted range at low ambient
temperatures...............................................................................................5
4.5 Engine on fire or fire in the engine
compartment ........................................................................................ 5
4.6 Trouble shooting ................................................................................... 6
Effectivity: 912 Serie
Edition 4 / Rev. 0
BRP-Rotax Page 4-1
November 01/2016

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