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Rotax 912 i series Service Manual

Rotax 912 i series
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BRP-Rotax
MAINTENANCE MANUAL LINE
Points of Inspection
Interval Operating hours Chapter
Reference
Signa-
ture
* no periodic maintenance require-
ment after the first 25 hours of
operation
25* 50 100 200 600 1000
on radiator cap and/or if the coolant
manufacturer requires a change
interval.
Flushing the
cooling
system
18) Engine cleaning
Engine cleaning. X X X X X 12–20–20
Engine
cleaning
19) Liquid level check
Verify liquid level, replenish as
necessary.
X X X X X 12–10–00
Fluid
capacities
20) Engine test run
Observe the safety instructions!
Start the engine and run to operating
temperature.
Limits see Operators Manual 912 iS.
Ignition check at _____ rpm engine
speed. Speed drop without LANE:
A (Off)___________rpm
B (Off)___________rpm
A/B (difference)________rpm
Checking the idle speed.
After engine test run, re-tighten the oil
filter by hand (only at cold engine).
Checks for leaks.
X X X X X 12–20–00
Test run of
engine
Returning engine to service
On the engine identified as per point 5, on the ___________________________the________hr.
Check at______hr. (TSN___, TSO___) was carried out according to recommendations of the engine manu-
facturer and was recorded in the Engine Log book.
Location, Date_______________________
Inspector___________________________
Aircraft mechanic_____________________
Certificate No.______________________
Effectivity: 912 i Series
Edition 2/Rev. 0
05–20–00
Page 15
September 01/2018

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Rotax 912 i series Specifications

General IconGeneral
Number of Cylinders4
Max Power100 hp (73.5 kW)
Max Power Output RPM5800 rpm
Ignition SystemDual electronic ignition
Oil SystemDry sump, forced lubrication with separate oil tank
Reduction Gear Ratio2.43:1
TBO2000 hours
Engine Type4-stroke, horizontally opposed
Displacement1352 cm³
Bore x Stroke84 mm x 61 mm
Max Torque128 Nm
Fuel TypeAvgas 100LL or unleaded automotive gasoline
Fuel SystemElectronic fuel injection
Cooling SystemLiquid/air-cooled

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