Pipistrel VIRUS SW 600 D User Manual

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Virus SW 600 D
iS engine POH Supplement
SPOH-127-00-41-001
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SECTION 1
GENERAL
1.6 SYSTEMS
1.6.1 POWERPLANT
The engine installed is Rotax 912 iS Series providing 73.5 kW takeo power.
All limits as defined by the engine manufacturer apply. The engine can be
operated with AVGAS 100LL or MOGAS (min. RON 95 antiknock properties
and max. 10% ethanol content) as by Rotax specification. The propeller is
driven by a gearbox which is equipped with a Rotax slipper clutch.
The engine is both ram air and liquid-cooled, while a separate, oil-based
lubrication system provide some additional cooling.
1.6.3 FUEL SYSTEM
The airplane has two integral tanks located in the left and right wing. Collec-
tor tanks are present downstream from the main tanks and a fuel selector
with three dierent positions: LEFT, RIGHT and OFF. Maximum usable fuel
quantity is 2 x 35.6 kg / 2 x 49.5 L (2 x 36 kg / 2 x 50 L max tank capacity).
The fuel system incorporates with two electrical pumps (main and auxiliary)
positioned in the baggage compartment. A gascolator that removes water
from the fuel system is present, equipped with filter and drain.
See Section 7 – Airplane description for additional details.

Pipistrel VIRUS SW 600 D Specifications

General

Brand	Pipistrel
Model	VIRUS SW 600 D
Category	Aircrafts
Language	English