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Icarus Foundation

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F109 Low wing aircraft ,for school and cross country

f109.jpg

    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)

 

f109lat.jpg

     Data - Performance

 
ULM Version:
Max take-off weight : 450 Kg (992 lb)
Empty weight : 275 Kg (605 lb)
Stall speed with flaps : 65 Km/h (40 Mph)
Cruise speed : 235 Km/h (146 Mph)
Max.horizontal speed : 260 Km/h (162 Mph)
Vertical speed : 6.5 m/sec ( 1280 ft/min)
Max.flight distance with 2 pilots : 1200 Km (748 Miles)
Engine : Rotax 912 100HP


 LSA-ELA Version
Max.take-off weight : 600 Kg (1320 lb)
Empty weight : 310 Kg (680 lb)
Stall speed with flaps : 72 Km/h (45 Mph)
Cruise speed : 240 Km/h (150 Mph)
Max.horizontal speed : 270 Km/h (168 Mph)
Vertical speed : 5 m/sec (985 ft/min)
Max. flight distance with 2 pilots : 1450 Km (900 Miles)
Engine :Rotax 912 100HP



  
  
 

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