Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 45 of 73
12.3 Cruise Speed (Single Seated)
Rotax 912 UL Rotax 912 UL S
C42 à 4700 trs/min (65%)
155 km/h (84 kts) 165 km/h (89 kts)
C42B à 4700 trs/min (65%)
160 km/h (86 kts) 170 km/h (92 kts)
C42C à 4700 trs/min (65%)
165 km/h (89 kts) 175 km/h (94 kts)
C42CS à 4700 trs/min (65%)
175 km/h (94 kts) 185 km/h (99 kts)
Speed for a maximum range:
140 km/h (76 kts) 145 km/h (78 kts)
Maximum range with a 50l tank with no wind :
approx. 270 nm (500 km)
Maximum range with a 65l tank with no wind :
approx. 350 nm (650 km)
12.4 Performance with Engine Shut Down
(Single Seated)
Maximal Take-off mass: 472.5 kg
Minimum sink rate: 2 m/s (393 ft/min)
à 85 km/h (46 kts) with flaps in position II
Best glide raio 1 :11
à 95 km/h (51 kts)
ATTENTION :
Follow the instructions in the ROTAX operator’s manual.
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