Rotax 912 Series Service Manual

Effectivity 912/914 Series
Edition 1 / Rev. 0
74-00-00
page 13
May 01/2007
d02624
BRP-Rotax
Maintenance Manual
00397
Fig. 74-7
6
1
2
3
4
5
- Check all cables and their plug connections for damage and correct
connection as per wiring diagram. See 74-00-00 sec. 3.13.
- Check all plug- and screwed connections for oxidation and tight fit.
- Check shorting cables and ignition switch. If ignition switch failure is
suspected, the shorting cable can be pulled off the ignition switch.
▲ WARNING: Proceed with particular care, because the ignition is not switched
off.
- Assure sufficient grounding between engine, battery and fuselage. Observe
the fuselage manufacturer's wiring diagram.

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