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Rotax 914 series Installation Manual

Rotax 914 series
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page 88
July 01/2008
Effectivity: 914 Series
Edition 2 / Rev. 0
d04279
INSTALLATION MANUAL
BRP-Rotax
CAUTION: Employ GENUINE-ROTAX
fuel pumps only. Non-compliance
will release BRP-Rotax from any liability.
Place of installation:
- Installation of the fuel pumps principally near the fuel tank to gain
advantage of a cool location, especially important at tendency of vapour
locks.
- Install the pump in low position, if possible below fuel tank, free of
vibrations. Therefore, fuel pump attached directly on the engine is not
permitted.
Max. suction head 250 mm (10 in).
WARNING: Certification to the latest requirements such as FAR or EASA
has to be conducted by the aircraft manufacturer.
Because of the risk of steam vapour formation on the suction side of the
pumps and other safety reasons is the pump installation not permitted in the
engine compartment.
WARNING: Installation of the fuel pumps in the engine compartment
and in the cockpit is not permitted since the fuel pumps
are not of a fire resistant construction.
WARNING: Should the situation arise, certification to the latest require-
ments such as FAR or EASA would have to be conducted by
the aircraft manufacturer.
- If possible the fuel pump should be installed in such a way that it is easily
accessible for maintenance (so that the fine filter (1) can be checked
according to the maintenance schedule)
Fig. 50/1
00157
1

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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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