2023 New ICP Aviazione Ventura 4 Experimental Ultralight

Description

• The kit has been reviewed by the FAA, ENAC, IAA, South African CAA & many other Civil Aviation Authority in Europe & all over the world & it has been found eligible for licensing in the Experimental Amateur-Built category. This means that the fabrication work we do on the kit components is less than 50% of the total required to complete the aircraft & that at least 51% of the work remains for the kit builder.
• By virtue of the new wing with Riblett GA 35-418 airfoil, The Ventura-4 can approach for landing as slow as 80 kph (50 mph/43 knots) at maximum weight & with its high propeller clearance, can operate from semi-prepared runways shorter than 250 meters with a large margin of safety. Combining such excellent STOL characteristics, typical of all ICP family aircraft, with high cruising speed & brilliant manoeuvrability with brisk roll response, the aircraft offers optimal performance in any situation giving the pilot full control & a lot of fun.
• The Ventura is an extremely versatile aircraft, & thanks to the large engine compartment it can be powered with a variety of solutions ranging from the compact Rotax 912 (recommended for the 2-seater version only) to the powerful 180 HP Lycoming IO-360. All this combined with a considerable payload (415 kg if equipped with Rotax 915 iS or 320 kg if with Lycoming IO-360).
• Structure
• The Ventura 4 is a monoplane type, with 4 seats, fitted with a high wing supported by struts.
• All metal structure with load resisting panels.
• High lift GA 35 418 Aerofoil with Junkers type flaperon (aileron + flap) with electrical control.
• Trim with electrical control on the elevator & with manual control on the rudder.
• Long range wing fuel tanks with 2×36 litres capacity in each wing. The tanks are connected & flow into a 18 ltr collection sump placed in the fuselage. A single drain valve at the bottom of the fuselage is provided for fuel sampling.
• Cockpit
• The two large removable lateral doors allow easy independent access to the cabin.
• Doors are fully transparent allowing good visibility.
• The cockpit is insulated, has upholstery covered seats & a fitted carpet.
• The cabin arrangement features two upholstery adjustable front seats & 2 rear upholstered seats.
• The luggage compartment situated behind the rear seats is accessible during the flight & can hold up to 20 Kg (45 lbs).
• The cabin’s ventilation is provided by cabin adjustable air scoops on the side of the forward fuselage. A dynamic air scoop intended to extract the cabin air is fitted at the top of the baggage compartment.
• Heating system can be orientated on feet or on windshield with control on the dashboard.
• Cabin light.
• Standard Instruments
• Instrument panel completely customizable by the customer.
• By default we provide the basic analogue instrumentation to be able to fly (Air speed indicator 3 1/8” with coloured arcs, Altimeter 3 1/8” with setting window, Vertical speed indicator 3 1/8”, Magnetic Compass, Slip & skid indicator, as well as engine instruments if compatible)
• The wide panel lends itself well to house the latest generation digital instrumentation.
• Engine
• Rotax any of the 900 series
• Lycoming up to 180 Hp
• Propellers
• Constant speed or pitch fixed
• Dimensions
• Wingspan – 9 m
• Wing Area – 13.5 sqm
• Length – 7.3 m
• Height – 2.8 m
• Cabin Width – 1.16 m
• MTOW – 800 kg
• Payload – 320-415 kg
• Seats – 4
• Fuel
• 4x 36 lts + 18 lts collector tank
• Speeds
• Stall – 76 km/h
• Cruise – 220 km/h
• VNE – 260 km/h
• Distances
• Take off run – 210 m
• L&ing run – 260 m