Ikarus Breezer

Low wing airplane in aluminium/mixed construction, made in Germany.

The Breezer is an aerodynamically controlled ultralight-aircraft. It is designed to be an aircraft for travelling and sports purposes. The high grade flight quality makes it advantageous not only for private persons but also for clubs and flight schools.

To fly fashionable with a well-engineered technology at a fair price/performance ratio.

  • Fuselage and wings made of aircraft-aluminium
  • Cowling, upper part of fuselage and wingtips made of glass fibre
  • Cockpit-hood to be opened to the rear
  • Easy access from the front
  • Hinged wings optional
  • Tricycle undercarriage
  • Steerable nose-wheel
  • Twin-controls, ailerons and elevators via control stick

The Breezer is to be delivered as a ready-built or a kit for individual build

Construction
  • Low wing airplane made of aluminium /mixed construction
  • Two-seater (side-by-side)
  • Undercarriage with 3 wheels, nose wheel steerable
  • Main gear glass fibre
  • Conventional 3-axes steering
  • Flaps, ailerons, elevators, rudder
Powerplant
  • 4-cylinder-4-stroke liquid-cooled / air-cooled engine with opposed cylinders Rotax 912 UL version, 58 kW/80 HP, including electrical starter, electronic dual ignition, integrated reduction gearbox, carburettor preheating or optional Rotax ULS 74 kW/100 HP
  • Ground-adjustable 2-blade carbon-fibre propeller
  • Spinner (Glass fibre)
  • Stainless steel exhaust system
Standard equipment
  • Covering aluminium, clenched, caulked, metallic finish; glass fibre parts (motor cowling, upper fuselage, wingtips): red or blue
  • Upholstery for seats, cockpit and luggage area made of high-value textile
  • Lockable cockpit-hood (dyed blue) with fresh air inlets left and right
  • Cabin heating
  • Luggage area behind the seats
  • Hydraulic disk brakes via brake lever in the console
  • Parking brake
  • Elevator trim
  • 12 V plug
  • Flight instruments:
    Altimeter , Speed indicator , Compass, Vertical speed indicator, bank indicator
  • Motor instruments:
    RPM indicator, oil pressure indicator, CHT gauge, oil temperature gauge, fuel gauge

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
 useful load
gross weight
fuel capacity
range		 80 hp
x
 6,49 m
 2,12 m
8,71m
11,85 sqm
2
 281 kg
 191,5 kg
 472,5 kg
 x70 Litres
 900 km		 100 hp
x
 6,49 m
 2,12 m
8,71m
11,85 sqm
2
 281 kg
 191,5 kg
 472,5 kg
 70 Litres
 900 km

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
 service ceiling		 135 m
 x
x
 185 km/h
 140 m
x		 95 m
x
x
 200 km/h
 140 m
x

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed 		x
 245 km/h
 65 km/h
x		 x
 245 km/h
 65 km/h
x

All specifications are based on manufacturer's calculations