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Rotax 914 series Maintenance Manual

Rotax 914 series
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76-00-00
page 52
May 01/2007
Effectivity 914 Series
Edition 1 / Rev. 0
d02626
BRP-Rotax
Maintenance Manual
3.1.2.8) Circuit breaker for servo motor
See Fig. 76-49.
The location of the circuit breaker (1) depends on the aircraft
type, but is limited by the length of the wiring harness.
â–  CAUTION: The circuit breaker is not included in the
delivery range of the engine. Check circuit
breaker according to the aircraft manufactur-
ers instructions.
- Operational test of circuit breaker:
1) - circuit breaker closed
- switch on TCU
The servo motor self test is performed.
2) - circuit breaker open
- switch on TCU
No self test of servo motor is performed.
With the circuit breaker open, the servo motor must not start
turning. The orange caution lamp starts flashing.
â–  CAUTION: If the required boost pressure cannot be
reached or if the circuit breaker does not act
correctly, locate the cause. Until the cause
has been found and rectified, engine opera-
tion is only permitted for ground testing.
â–  CAUTION: In the event of physical damage or incorrect
operation, replace the part without delay.
M
214
TCU
00217
1
Fig. 76-49

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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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