2-person ULM aircraft Savannah™ VG
4-stroke enginetouristsingle-engine

2-person ULM aircraft
2-person ULM aircraft
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Characteristics

Number of seats
2-person
Motorization
4-stroke engine
Applications
tourist
Other characteristics
single-engine
Length

6.3 m
(20'08" )

Height

2.6 m
(8'06" )

Wingspan

9 m
(29'06" )

Wing surface

12.9 m²
(138.9 ft²)

Empty weight

282 kg
(622 lb)

Max. take-off weight

450 kg
(992 lb)

Fuel capacity

78 l
(20.6 gal)

Maximum speed

192 km/h
(119 mph)

Cruise speed

173 km/h
(107 mph)

Stall speed

55 km/h, 59 km/h
(34 mph, 37 mph)

Take-off distance required

55 m
(180'05" )

Landing distance required

70 m
(229'07" )

Description

The Savannah™ VG (Vortex Generator) was born from the need to have an aircraft with STOL qualities, made equal to the model Savannah, but with a substantial increase of the cruise speed and the maximum one. This aircraft is very well-finished and equipped with various production accessories and optional. The aim of the little vortex generators stuck on the wing’s leading edge, is to energize the boundary layer. The result is a decrease of the stall speed due to a bigger wing attachment’s angle, as well as an increase of the control authority. The Savannah™ VG is the ideal aircraft for those who want to combine the safety of the STOL flight with the possibility to do long transfers with a cruise speed higher than 170 Km/h. The cockpit completely sound insulated and heated increase the comfort already in basic version. As for the standard Savannah, also the VG version assures an extreme versatility, thanks to the possibility to choose it in different configurations: tricycle landing gear or tail-wheel gear or amphibian. StructureClick to show – The Savannah™ VG is a monoplane type, with two side-by-side seats, fitted with a high wing supported by struts. – The airframe structure is a full-metal one with load-resisting panels. – The wing presents a “high lift” NACA 650-18 modified airfoil with Junkers type flaperon (aileron + flap) with manual or electrical (optional) control. – The squared fuselage and the dorsal fin are fitted to improve the directional. – Trim with electrical control on the elevator and with manual control on the rudder. – It is possible to install a parachute “Junkers 500” type

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Exhibitions

Meet this supplier at the following exhibition(s):

AERO Friedrichshafen 2024
AERO Friedrichshafen 2024

17-20 Apr 2024 Friedrichschafen (Germany) Hall Vide - Stand B3-202

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    *Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.