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Rotax 914 series Installation Manual

Rotax 914 series
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Effectivity: 914 Series
Edition 2 / Rev. 0
d04275
page 31
July 01/2008
BRP-Rotax
INSTALLATION MANUAL
9) Preparations for engine installation
CAUTION: The stated directives are measures to pay CAUTION to at engine
installation to prevent any accidents and engine damage.
9.1) Transport
The engine to be lifted by two hooks or straps around the middle of the intake manifolds.
See section engine views, numbering of cylinders and definition of main axes.
9.2) State of delivery
It is possible to mount the engine to a palet using steel angles.
CAUTION: The attachment screws are only for transport and must not be used in
the aircraft.
9.3) Engine preservation
The engine is preserved at BRP-Rotax thus warranting proper protection against
corrosion for at least 12 month after date of delivery from BRP-Rotax.
This warranty is subject to the following conditions:
- the engine has to be stored in the packing as supplied by BRP-Rotax.
- the covers on various openings must not be removed (see section of protective
covering)
- engine has to be stored in a suitable place (at min. - 40 °C (- 40 °F) and max.
+ 80 °C (+ 176 °F)).
If the engine is stored for a period longer than 12 month perform every 3 months the
tasks given in the current valid Maintenance Manual, section 11.11.1 "Preservation of
a new engine".

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Rotax 914 series Specifications

General IconGeneral
Bore79.5 mm
Stroke61 mm
Compression Ratio9.0:1
Cooling SystemLiquid-cooled cylinder heads, air-cooled cylinders
Redline5800 rpm
Engine Type4-cylinder, 4-stroke
Fuel TypeAvgas 100LL
Oil SystemDry sump
Fuel Systemfuel injection
TBO (Time Between Overhauls)2000 hours
Displacement1.211 liters (1211 cc)
Power Output84.6 kW (115 hp) at 5, 800 rpm

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