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5.1. Introduction
The information in stalling speed and other performances of the ATEC 212 SOLO with
ROTAX 912 UL 80 HP and propeller FITI ECO COMPETITION 2b/168.
5.2. Stalling Speeds (CAS)
Engine idling Flaps retracted Flaps I (10°) Flaps II (20°) Flaps III (35°)
72 km/h …39 kt 65 km/h ... 35 kt 63 km/h ... 34 kt 62 km/h ... 33 kt
Engine stopped 75 km/h ... 40 kt 67 km/h ... 36 kt 65 km/h ... 35 kt 64 km/h ... 35 kt
5.3. Take off Distance at 15 m / 50 feet height
Runway surface Take off distance
Concrete 190 m … 620 ft
Turf 215 m … 700 ft
5.4. Rate of Climb
Air speed Rate of climb
120 km/h … 65 kt 8,5 m/s … 1700 FPM
140 km/h … 75 kt 8 m/s … 1600FPM
5.5. Cruising Speeds
ROTAX 912 UL 80 HP
Air speed (IAS) RPM Fuel consumption
120 km/h … 64,8 kt 3000 4,8 l/h … 1,26 USGPH
140 km/h … 75,6 kt 3350 6,2 l/h … 1,64 USGPH
160 km/h … 86,4 kt 3650 8,0 l/h … 2,11USGPH
180 km/h … 97,2 kt 3950 10,0 l/h … 2,64 USGPH
200 km/h … 108 kt 4270 12,2 l/h … 3,22 USGPH
220 km/h … 119 kt 4600 14,8 l/h … 3,91 USGPH
240 km/h … 130 kt 5020 17,8 l/h … 4,70 USGPH
260 km/h . . .140 kt 5350 21,0 l/h .....5,55 USGPH
280 km/h .....150 kt 5600 24,5 l/h .....6.47 USGPH
5.6. Range of Flight
Air speed (IAS) Range of flight 30 min. flight reserve
140 km/h … 75,6 kt 1036 km … 560 nm 3,1l … 0,82 USG
160 km/h … 86,4 kt 900 km … 486 nm 4,0 l … 1,05 USG
180 km/h … 97,2 kt 792 km … 428 nm 5,0 l … 1,3 USG
200 km/h … 108 kt 703 km … 380 nm 6,1 l … 1,6 USG
220 km/h … 119 kt 618 km … 334 nm 7,4 l … 2,0 USG
240 km/h … 130 kt 539 km … 291 nm 8,9 l … 2,3 USG
260 km/h.....140,5 kt 476 km .....257 nm 10,5 l .....2,77 USG