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The CT2K is built completely with carbon fiber technology.
Instead of having a Gel coat finish (which is not UV resistant),
the CT2K has a 2 component polyurethane finish which is highly
resistant to UV exposure and very durable.
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Carbon fiber aircraft construction offers great advantages in
terms of strength, durability, weight-savings,
corrosion-resistance, and fatigue-resistance. For these reasons,
this modern method of aircraft construction has become
increasingly popular for civilian, military and commercial
aircraft – as well as for airliners – with carbon
fiber being used for complete aircraft or simply for
highly-stressed structural components. The use of carbon fiber
for aviation is increasing very rapidly, despite the
substantially higher costs of carbon fiber construction compared
to conventional aluminum/rivet construction.
A modern airplane should be built with modern
technology!
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ENGINE DATA
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Rotax 912 80 HP / 5,800 rpm
Rotax 912S 100 HP / 5,800 rpm
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TRAVEL
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Over East Prussia with seven CT´s
flying to Litauen and back.
2,500km in 4 days.
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The further you fly -- the more the CT2K superiority
shows!
The CT2K has a 2,000 km range and has large luggage
compartments that can fit everything for your trip: whether
packing a tent and camping gear, or taking your luggage for your
trip to attend the opera! During your flights, the very roomy
cabin and comfortable seats will make flights throughout Europe a
wonderful possibility on weekends and holidays.
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PERFORMANCE
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Vso (minimum speed)
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62 km/h IAS (with wing tips) 65 km/h IAS (without wing
tips)
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VNO: green arc 270 km/h IAS
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270 km/h IAS
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VCR 75%: With 912 (75% = 60 HP)
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225 km/h IAS*
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VCR75%: With 912S (75% = 75 hp)
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235 km/h IAS*
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VNE: Maximum airspeed (red line)
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310 km/h IAS
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take-off run
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90 m
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take-off distance over 15 m obstacle
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160 m
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range with 130 l (30 min reserve)
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2.000 km
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climbing performance 80 HP / 100 HP
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3,5 / 5 ms
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* data for CT2K with Wingtips in 1,000 ft. ICAO standard
atmosphere with wheel pants and landing gear strut fairings and
variable fixed-pitch prop.
** US-Version allows maximum speed 210 km/h, because of
different engine and propeller configuration.
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Explanations concerning rated speeds:
- VNE 310 km/h may be given with maximum application of 1/3
rudder
- VNO 270 km/h is the max. permitted cruising speed according
to German BfU 95 certification standard.
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TESTED BREAK LOAD FACTORS
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With 450 kg take-off weight
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9.6 g
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With 560 kg take-off weight
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7.7 g
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With 600 kg take-off weight
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7.2 g
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Max. altitude
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14.000 ft
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Minimum empty aircraft weight (approx.)
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262 kg
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Maximum take off weight*
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600 kg
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Minimum single pilot weight
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60 kg
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Wing area
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10.8 m2
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Wingspan
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9.3 m
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Overall height
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2.16 m
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Overall length
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6.22 m
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Max. cabin interior width
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1.24 m
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Fuel capacity
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130 l
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* Limited by different certification rules in different
countries
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- adjustable seats (fits taller or shorter pilots)
- four-point shoulder/seat belts
- three-colour interior lacquer finish
- two baggage compartments (accessible from inside or outside
the cockpit)
- two small storage compartments inside the cockpit
- large cockpit with easily removable instrument panels
- especially wide cabin doors
- one-piece windshield
- one-piece door window
- conventional three-axis dual controls
- manual elevator trim
- electrical flaps system -12° to +40°
- keyed ignition with electric starter
- engine: Rotax 912 with 80 HP or 912S with 100 HP
- advanced design two-blade propeller
- 130 litres fuel capacity
- tricycle landing gear
- main wheels 6,00-4 with hydraulic disc brakes
- nose wheel 5,00-4 steer able
- flight manual
- instruments included:
o airspeed indicator to 320 km/h
o altimeter with adjustable hPa/mbar scale
o magnetic compass with deviation chart
o slip indicator
o tachometer
o oil pressure gauge
o oil temperature gauge
o cylinder head temperature gauge
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