|Vmin minimum speed||65 km/h IAS*|
|VCR: cruising speed (green arc)||240 km/h IAS*|
|VC 75%: with 912 (75% = 60 PS)||230 km/h IAS*|
|VC 75%: with 912S (75% = 80 PS)||240 km/h IAS*|
|VNE: max. permissible airspeed (red line):||301 km/h IAS**|
|Take-off run||90 m|
|Take-off distance over 15 m obstacle||160 m|
|Max. range ability with 130 l by 180 km/h (30 min reserve)||2.000 km|
|Tested break load|
|With 450 kg take-off weight||9.6 g|
|With 600 kg take-off weight||7.2 g|
|Weights and Dimensions|
|Minimum single pilot weight||60 kg on one seat|
|Min. Empty aircraft weight (approx.)||ca.268 kg|
|Max. take-off weight||600 kg depends on country regulations|
|Wing area||CT2K 10,8 m2 CTSW 9,8 m2|
|Wingspan||CT2K 9,3 m CTSW 8,55 m|
|Overall height||2,16 m|
|Overall length||6,22 m|
|Max. cabin interior width||1,24 m|
|Tank capacity||130 l|
*Data for CTSW in German LTF-UL version with 472,5 kg MTOW , CT2K is
ca. 5 km/h slower. Values are for ICAO standard atmosphere with put
into operation engine and non adjustable fixed pitch propeller.
**In Germany and Austrian limited to 260 km/h through rescue system.
Explanations concerning speed rates:
VNE 301 km/h, from VA to VNE only 1/3 rudder may be given maximum application.
VCR 240 km/h is the max. permitted cruise speed according to German LTF-UL 2003 certification standard.