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Ikarus C42

 

 

 

The Lightsport Mall
  

Fuel @ cruise consumption 3 US gallons/hr
   
M.A.U.W.1141lbs

Empty

593

lbs

Pay load

548

lbs

 

 

 

Max Fuel

17.5 Gallons

Optional extra tank

17.5 Gallons

 

 

 

 

 

 

Climb rate 100hp @ M.A.U.W

1100 fpm

 

Climb rate 80hp @ M.A.U.W

900 fpm

 

 

 

 

 

 

 

Cruise 80hp   80kts

 

 

Cruise 100hp   85kts

 

 

 

 

 

Max speed 80hp 105kts

 

 

Max speed 100hp 110kts

 

 

 

 

 

 

 

 

Stall speed  (no flap) 40kts

 

 

 VNE, Never Exceed Speed:

 139 mph

121 kt 

VA Max. maneuvering speed94 mph82 kt
VS0 Stall speed, full flaps38 mph33 kt
VS1 Stall speed, flaps retracted48 mph42 kt
VFE Max speed72 mph63 kt
   
Areas:  
Wing area135 sq ft12.5 sq.m
Cabin width48 inches 
 
 
 

The C42E  is an innovative modern two seat airplane that is setting new standards. Over 680of these comfortable, affordable and go anywhere aircraft are now flying in and around the world.

They are built by Comco Ikarus in Germany – a company widely recognized for its quality aircraft. Comco has been in existance since 1970 and has produced over 2500 C22s prior to the C42. The Ikarus C42E offers superior handling characteristics as well as stability and ease of control both in the air and on the ground. Low operating costs, keep the cost of ownership down to a minimum.  The C42E now has a higher gross weight.  Improvements for the LSA markets.  

Put the fun back into flying.

You will fly more hours at a lower cost in the C42E

“Like to try it” – ”Come and fly it”

Awards
World Championships 1997 (First World Air Games)
World Speed Record 1998 (500 km closed circuit)
Winner of the German Championships 1996, 1999, 2000 and 2001
World Speed Record(100 km)

Standard Equipment for C42E

Construction:

  • Fuelage Covering : Glass fibre, Aramid, Carbon fibre
  • Fuselage, Wings, struts and empennage are of high-strength aluminium-tubing
  • Undercarriage with 3 wheels
  • Fittings and screws are of stainless steel or of high-strength standard elements
  • High-tech cover (UV stabilized) for wings and empennage
  • High-lift flaps with separate ailerons
  • Removeable Wings
Engine:
  • 4 cylinder, 4-stroke liquid-cooled/ air-cooled Rotax 912 UL2 opposed-cylinder engine 58 kW/ 80 hp, with electrical starter, dual electronic ignition, carburetor preheating, integrated reduction gear box
  • Exhaust system made of high tensile steel (serial standard)
  • 3-blade Neuform (Glass fibre/Carbon), ground adjustable
  • Spinner (Glass fibre)
Standard Equipment
  • Hydraulic disk brakes with parking brake
  • Special light weight battery
  • External antenna for radio, installed with cables
  • 12 Volt plug
  • On stick electric elevator trim
  • Nose Landing light
  • Tail mounted Strobe
  • Tank, fuel capacity 17 US Gallons
  • Cabin Heating
Flight instruments:
  • Altimeter
  • Air speed indicator
  • Compass Silva
  • Bank indicator
Engine instruments:
  • RPM indicator, oil pressure indicator
  • CHT gauge
  • Oil temperature gauge
  • fuel gauge
  • Hour Meter
Standard Features
  • All surfaces in white color
  • Cabin inside in dark grey color
  • Cabin windows and windshield Makrolon
  • Cushion for the seats (black/blue or black/red)
  • Door map pockets left and right
  • Gas-pressure spring assembly for cabin doors
  • Door locks left and right  
  • Composite wing tips
  • Adjustable fresh-air inlets in doors