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Rotax 914 series Installation Manual

Rotax 914 series
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page 134
July 01/2008
Effectivity: 914 Series
Edition 2 / Rev. 0
d04283
INSTALLATION MANUAL
BRP-Rotax
23.2) Sensor for oil temperature
See Fig. 91/92
- location: oil pump housing
- marking (2): marked with "TO" (temperature oil) on oil pump flange
CAUTION: To avoid any mix-up with indication wiring, mark this particular cable
also with "TO".
- position of the temperature sensor (1) on the oil pump flange:
Fig. 91
TO
Fig. 92
12010080604020 140 160
1200
1000
(
Ω)
(°C)
800
600
400
200
0
- connection of sensor wiring: spade terminal 6,3 x 0,8 to DIN 46247
- grounding: via engine block
- graph of sensor resistance over temperature
CAUTION: The graph resistance over temperature has been determined, and is
effective at the following conditions only.
ambient temperature: 20 °C (68 °F)
tolerance: ± 15%
BRP-Rotax offers a non-certified temperature indicating instrument. Refer to Illustrated
Parts Catalog, latest issue.
WARNING: Certification to the latest requirements such as FAR of EASA has to be
conducted by the aircraft manufacturer.
00226
00227
04869
Axes
x axis
mm
y axis
mm
z axis
mm
-115 46 -150
point of
support
1
2

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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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