Aircraft Type: CTSW
FLIGHT DESIGN
Aircraft Operating Instructions
Page: 6-1
AU 010 01000
Rev. No: 7
Original Issue Date: 28-Feb-2005
Revision Date: 29-Apr-2008
6 Performance
The performance figures are based on sea level, standard atmospheric conditions and a
gross weight that depends on your local certification rules.
6.1 Takeoff distance
600 kg 472,5 kg
Take-off distance over a 15 m / 50ft obstacle 232 m / 760 ft 186 m / 610 ft
6.2 Best rate of climb
At weight 600 kg and flaps 0°: VY = 154 km/h / 78kts
6.3 Best angle of climb
At weight 600 kg and flaps 0°: VX = 122 km/h / 66 kts
6.4 Cruise speed
Propeller type: Neuform, 2 blade, 1650 mm dia.
Propeller blade incidence at 3/4*r: 27 deg
Cruise speed at 75% power
600 kg
-6° (-12°)
205 km/h / 112 kts
472,5 kg
-12°
205 km/h / 112 kts
6.5 RPM
Minimum Idle: 1400
Static: 4700
Normal climb: 4800
Maximum: 5800 (5 min)
Max. continuous: 5500
Normal cruise: 4200 – 5200
Cruise @ 75%: 5200
6.6 Fuel consumption
Fuel consumption in l/h / U.S. gal/h Rotax 912 UL2 Rotax 912 ULS
at take-off performance 24,0 / 6,3 27,0 / 7,1
at max. continuous performance 22,6 / 5,6 25,0 / 6,6
at 75% continuous performance 16,2 / 4,3 18,5 / 4,9
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