DOVA AIRCRAFT DV-1 SKYLARK, Руководство по обслуживанию

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Power plants:
Aircraft is powered by ROTAX 912UL and ROTAX 912ULS mostly. The engine is attached through shock
absorbers to engine bed welded from steel rods. The engine bed is attached to firewall through
strengthened points. The engine compartment is covered with two fiberglass cowlings (lower and upper
one). Cowlings are one-side painted to match the aircraft and they are both removable. The upper one is
attached with cam-locks.
Fuel system:
Two integral fuel tanks are mounted in wings, with 45L volume each. They are made from duralumin
sheets riveted and sealed together. Each fuel tank is equipped with filling intake, outlet valve, sludge valve,
air-bleeding valve and fuel-meter. Fuel system itself is equipped with three-ways fuel valve, fuel filters and
electrical fuel pump.
Interior:
Aircraft is equipped with two upholstered seats placed side-by-side. Position of each seat is adjustable
with position lock. Further equipment are four-point safety belts, baggage compartment placed behind
the seats and safety net for fixing luggage.
Canopy:
Canopy is made from one single part of organic glass. This glass is riveted and glued to welded frame from
duralumin tubes. Canopy opens with forward sliding movement. Canopy frame is attached to fuselage
through metal pull-out system. The canopy latch is placed in the top of the canopy and it is lock-able.
Ventilate system:
Ventilation is provided through rounded valve in front of the canopy. As an option, there are side sliding
windows.
Electrical installation:
Electrical system is single phase 12V system with negative pole grounded. As a source, there is a duty-free
battery and engine alternator. Each electrical circuit is protected with fuse or circuit breaker placed on
instrument panel.
Labels:
Ready-to-fly aircraft delivered from manufacture is equipped with given labels. In case of kit the labels are
delivered, but the owner had to placed them into correct positions. Warning: owner of the aircraft is
responsible for readability of the label during the aircraft lifetime.
Instruments:
Minimal instruments equipment:
- in-flight instruments: air speed indicator, altimeter, vertical speed indicator, slide-ball
indicator, compass, fuel gauges
- engine instruments: tachometer, oil temperature indicator, engine head temperature
indicator, oil pressure indicator
Radio: ICOM 200
Servo: for elevator trim surface Ray Allen T10A
Options: fuel pressure indicator, manifold pressure indicator, GPS AvMap EKP IV,
transponder Garmin , artificial horizon, landing light 100W.
Signal lights: position lights placed in winglets and strobe lights (2pcs in winglets ad
2pcs on fuselage)
Additional equipment:
There is a preparation for installation of ballistic rescue systems already provided.