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Rotax 914 series User Manual

Rotax 914 series
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Effectivity: 914 Series BRP-Powertrain page 1-5
OM Edition 2 / Rev. 0 April 01/2010
d04473.fm
1.4) Safety notice
Normal use z
- This engine is not suitable for acrobatics (inverted flight etc.).
- This engine shall not be used on rotorcrafts with an in-flight
driven rotor (e.g. helicopters).
- It should be clearly understood that the choice, selection and
use of this particular engine on any aircraft is at the sole dis-
cretion and responsibility of the aircraft manufacturer, assem-
bler and owner/user.
- Due to the varying designs, equipment and types of aircraft,
BRP-Powertrain grants no warranty or representation on the
suitability of its engine’s use on any particular aircraft. Further,
BRP-Powertrain grants no warranty or representation of this
engine’s suitability with any other part, components or system
which may be selected by the aircraft manufacturer, assemb
-
ler or user for aircraft application.
- Certain areas, altitudes and conditions present greater risk
than others. The engine may require humidity or dust/sand
preventative equipment, or additional maintenance may be re
-
quired.
- You should be aware that any engine may seize or stall at any
time. This could lead to a crash landing and possible severe
injury or death. For this reason, we recommend strict compli
-
ance with the maintenance and operation and any additional
information which may be given to you by your distributor.
WARNU
WARNING
Non-compliance can result in serious injuries
or death!
Never fly the aircraft equipped with this en-
gine at locations, airspeeds, altitudes, or oth-
er circumstances from which a successful no-
power landing cannot be made, after sudden
engine stoppage.
WARNU
WARNING
Non-compliance can result in serious injuries
or death!
Unless correctly equipped to provide enough
electrical power for night VFR (according la-
test requirement as ASTM), the ROTAX
914 UL is restricted to DAY VFR only.

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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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