Rotax 912 Series Service Manual

76-00-00
page 28
May 01/2007
Effectivity 914 Series
Edition 1 / Rev. 0
d02626
BRP-Rotax
Maintenance Manual
◆ NOTE: Figs. 76-21 and 76-22 show program version
TLR V4.3A.
◆ NOTE: The printer must be connected with the PC via
the parallel interface (1).
d) End of program
- Stop communication program with “Q” for QUIT
- Turn off the TCU
- Disconnect (store dongle properly)
- Switch off PC
3.1.1.5) Checking the components of the turbocharger control
The communication program allows quick detection of short-
comings of the components via the sub program „MONITOR“.
◆ NOTE: A corresponding trouble shooting chart is avail-
able on request from authorized distributors
and service centers. See latest Operators
Manual for the respective engine type or the
official Homepage www.rotax-aircraft-
engines.com.
Fig. 76-23
00196
1

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