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2-person ULM aircraft F109
piston enginesingle-engine

2-person ULM aircraft - F109 - Icarus Foundation - piston engine / single-engine
2-person ULM aircraft - F109 - Icarus Foundation - piston engine / single-engine
2-person ULM aircraft - F109 - Icarus Foundation - piston engine / single-engine - image - 2
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Characteristics

Number of seats
2-person
Motorization
piston engine
Other characteristics
single-engine
Empty weight

275 kg
(606 lb)

Max. take-off weight

450 kg
(992 lb)

Cruise speed

235 km/h
(146 mph)

Description

We started the fabrication of a new prototype,the low wing high performance aircraft F109. It's a classic all metal 2 place,with some distinct characteristics: - compound wing planform, having a very efficient laminar airfoil. - the main wing spar placed behind pilots seats,for good view when landing or take-off - sailplane-style wings joining inside fuselage,for 5min. assembly time - slotted flaps - differential ailerons,mixed with the flaps at take-off and landing - one-piece stabilator,with antiflettner and electric trimmer - fuel tank in fuselage behind the pilots, for quick and easy refill - adjustable rudder pedals - wide cabin for large people - 1.30m As EASA is preparing the ELA regulation ,inspired from the American LSA, we will produce two versions : European ultralight ULM (450 kg.MTOW) and European Light Aircraft ELA (600 kg.MTOW)
*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.