Rotax 912 i series Service Manual

BRP-Rotax
MAINTENANCE MANUAL LINE
Chapter: TOA
TABLE OF AMENDMENTS
Approval*
The technical content of this document is approved under the authority of DOA ref. EASA.21J.048
NOTE
THE APPROVAL IS GIVEN TO ALL CHAPTERS EXCEPT THE AIRWORTHINESS LIMITATIONS
SECTION 04-00-00 WHICH IS SUBJECT TO SPECIFIC APPROVAL OF THE EASA.
Cur-
rent
no.
Chapter
Page
Date of change Remark for
approval
Date of
approval
from
authori-
ties
Date of
inclusion
Signature
0 INTRO
all
Sept. 01 2018 DOA*
0 LEP all
Sept. 01 2018 DOA*
0
TOA
all
Sept. 01 2018 DOA*
0 00-00-00 all
Sept. 01 2018 DOA*
0 04-00-00 all
Sept. 01 2018 EASA approved
0 05-00-00 all
Sept. 01 2018 DOA*
0 05-10-00 all
Sept. 01 2018 DOA*
0 05-20-00 all
Sept. 01 2018 DOA*
0 05-50-00 all
Sept. 01 2018 DOA*
0 12-00-00 all
Sept. 01 2018 DOA*
0 12-10-00 all
Sept. 01 2018 DOA*
0 12-20-00 all
Sept. 01 2018 DOA*
Effectivity: 912 i Series
Edition 2/Rev. 0
TOA
Page 1
September 01/2018

Rotax 912 i series Specifications

General

Number of Cylinders	4
Max Power	100 hp (73.5 kW)
Max Power Output RPM	5800 rpm
Ignition System	Dual electronic ignition
Oil System	Dry sump, forced lubrication with separate oil tank
Reduction Gear Ratio	2.43:1
TBO	2000 hours
Engine Type	4-stroke, horizontally opposed
Displacement	1352 cm³
Bore x Stroke	84 mm x 61 mm
Max Torque	128 Nm
Fuel Type	Avgas 100LL or unleaded automotive gasoline
Fuel System	Electronic fuel injection
Cooling System	Liquid/air-cooled