C42 SERIES Pilot Operating Handbook
POH Issue 4 Rev. 5 Page 43 of 91
12.3 Cruising speed (solo)
At engine speed n = 4700 1/min
(65%) Rotax 912 UL Rotax 912 ULS
C42 84 kn (155 km/h) 89 kn (165 km/h)
C42B 86 kn (160 km/h) 92 kn (170 km/h)
C42E 86 kn (160 km/h) 92 kn (170 km/h)
C42C 89 kn (165 km/h) 94 kn (175 km/h)
C42CS 94 kn (175 km/h) 100 kn (185 km/h)
Speed for maximum range 76 kn (140 km/h) 78 kn (145 km/h)
Maximum range with 11 imp. fuel gallons (50 l)
tank capacity when windless approx. ............................... 270 nm (500 km)
Maximum range with 14.3 imp. fuel gallons (65 l)
tank capacity when windless approx. ............................... 350 nm (650 km)
C42CS ................................................................ approx.: 405 nm (750 km)
12.4 Engine off performance (solo)
MTOW ........................................................................... 1041 lbs (472.5 kg)
Minimum sink rate ............................................................ 393 ft/min (2 m/s)
At 46 kn (85 km/h), flap position II .................................... (take-off/landing)
Best glide angle ................................................................................ 1 to 11
At 51 kn (95 km/h) flap position I ..................................................... (cruise)
ATTENTION:
Follow the instructions in the ROTAX 912 operator’s manual.
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