C42E 540kg LSA POH Issue 3 China 15.03.2016
Page 21 of 36
5 PERFORMANCE
5.1 Takeoff distance to clear 15m, 50’ obstacle
Take off ground roll: 100m
Take off distance to clear 15m: 250m total at 54kt, half flap, Rotax 912ULS.
(Including ground roll)
5.2 Landing distance to clear 15m, 50’obstacle
Landing ground roll: 90m
Landing distance to clear 15m: 310m total at 54kt, full flap.
(Including ground roll)
5.3 Climb rate
Best climb rate: 930fpm Rotax 912ULS, at 66kt
Best angle of climb speed: 48kt
5.4 Cruise conditions
Because lightweight aircraft are more strongly affected by loading, conditions and propeller setting the
pilot is encouraged to plan very conservatively until experience is gained of his aircraft’s fuel consumption
at the conditions in which his aircraft is normally operated.
Typical economic cruise speeds lie in the range 80 to 115 mph (70 to 100 kt) with the 100 hp engine.
Note: This maximum speed applies only in smooth conditions with no turbulence. In turbulent
air, speed must be kept below V =110 mph (96 kt).
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