PreReg - 2019 DOVA SKYLARK

2019

DOVA

SKYLARK

PreReg

000

New

The DV-1 Skylark is designed for flight training, glider towing and recreational flights. Pricing: Factory build ready to fly aircraft: €75 000,00 (VAT excl) RTF DV-1 SKYLARK with Rotax 912 ULS (100 HP) KIT #1 DV-1 SKYLARK Quick build kit:€62 000,00 (Airframe kit with engine + canopy) Up to 150 hours required KIT #2 DV-1 SKYLARK Quick build kit: €45 000,00 Airframe kit NO engine + canopy Up to 200 hours required KIT #3 DV-1 SKYLARK Quick build kit: €41 000,00 (basic airframe kit from firewall to back) Up to 300 hours required

Semi-monocoque construction formed with reinforcements and duralumin skins. All structural parts are from duraluminium. The tail fin is an integral part of the fuselage. Control system welded parts are made from strength aviation steel L-CM3.3. Engine compartment is separated by stainless steel fireproof wall from cockpit. Equipped with ailerons and flaps with simple folding system assuring durable and reliable function and winglets made from fiberglass installed for better climbing performance. The wing is designed as self-supporting construction with main and auxiliary spars. Attached through three hinges into fuselage. The airfoil shape is formed by duralumin hardened leading and trailing edge ribs finally skinned with duralumin sheets. Empty weight 287 kg 290 kg Maximum take-off weight 450 kg (472.5 kg w/rescue system) 600 kg Useful load 163 kg 310 kg Fuel tanks capacity 90 l 90 l Maximum baggage weight 20 kg 20 kg Load factors in g’s (+4, -2) (+4, -2)

Two options of engine Rotax available – 912 UL (80 HP) / 912 ULS (100HP) The engine is attached to the engine bed which is suspended on the firewall. The cylinder heads are liquid cooled, and the cylinders are air cooled. Dry-sump forced lubrication system. Dual-electronic ignition. Engine equipped with electric starter, AC generator and the mechanical fuel pump. Fuel system consists of two wing integral tanks in total amount 90 liters (23,8 US gal), a fuel tank selector, a filter and a fuel pump on the engine. Each tank has a vent, drain valve fuel meter and filter in outlet valve. Engine Instruments: RPM indicator Air speed indicator (knots or km/h) Cylinder head temperature indicator (°C or °F) Altimeter (feet) Electric fuel indicator Magnetic compass Oil temperature indicator (°C or °F) Vertical speed indicator (ft/min or m/s) Oil pressure indicator (MPa or psi) Bank indicator Fuel pressure indicator Engine hours meter

Pilot operating handbook Maintenance manual Log book Set of aircraft test records

Tricycle landing gear with steerable nosewheel Canopy latch locking mechanism Metal fuel caps with lock Oil check cap in engine cowling

Four points safety points-belts (with shoulder straps) Fabric lined interior and upholstery seats Aft baggage compartment