DURABILITY

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.

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!

ENGINE DATA

Rotax 912 80 HP / 5,800 rpm

Rotax 912S 100 HP / 5,800 rpm

TRAVEL

Over East Prussia with seven CT´s flying to Litauen and back.

2,500km in 4 days.

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.

PERFORMANCE

Vso (minimum speed)

62 km/h IAS (with wing tips) 65 km/h IAS (without wing tips)

VNO: green arc 270 km/h IAS

270 km/h IAS

VCR 75%: With 912 (75% = 60 HP)

225 km/h IAS*

VCR75%: With 912S (75% = 75 hp)

235 km/h IAS*

VNE: Maximum airspeed (red line)

310 km/h IAS

take-off run

90 m

take-off distance over 15 m obstacle

160 m

range with 130 l (30 min reserve)

2.000 km

climbing performance 80 HP / 100 HP

3,5 / 5 ms

* 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.

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.

TESTED BREAK LOAD FACTORS

With 450 kg take-off weight

9.6 g

With 560 kg take-off weight

7.7 g

With 600 kg take-off weight

7.2 g

Max. altitude

14.000 ft

WEIGHTS AND DIMENSIONS

Minimum empty aircraft weight (approx.)

262 kg

Maximum take off weight*

600 kg

Minimum single pilot weight

60 kg

Wing area

10.8 m2

Wingspan

9.3 m

Overall height

2.16 m

Overall length

6.22 m

Max. cabin interior width

1.24 m

Fuel capacity

130 l

* Limited by different certification rules in different countries

STANDARD EQUIPMENT

• 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