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°) | |
| 72 km/h …39 kt | 65 km/h ... | 35 kt |
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Engine stopped | 75 km/h ... 40 kt | 67 km/h ... | 36 kt |
Flaps II (20°)
63 km/h ... 34 kt
65 km/h ... 35 kt
Flaps III (35°)
62 km/h ... 33 kt
64 km/h ... 35 kt
5.3.Take off Distance at 15 m / 50 feet height
| Runway surface |
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| Take off distance | ||
| Concrete |
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| 190 m … 620 ft | |
| Turf |
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| 215 m … 700 ft | |
5.4. | Rate of Climb |
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| Air speed |
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| Rate of climb | |
| 120 km/h … 65 kt |
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| 8,5 m/s … 1700 FPM | ||
| 140 km/h … 75 kt |
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| 8 m/s … 1600FPM | ||
5.5. | Cruising Speeds |
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ROTAX 912 UL 80 HP |
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| 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 |
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| 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 | |
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