Aquila (A 210)
AT01 (А 210) - легкий двухместный, с рядным расположением пилотов, однодвигательный самолёт, низкоплан нормальной аэродинамической схемы, предназначенный для воздушных путешествий, тренировочных полётов и буксировки.
Двигатель
| Bombardier Rotax 912S | ||
|---|---|---|
| Cylinders | 4 | |
| Engine power | 100 PS | 73,5 kW |
| Max. take off power and max. continuous power A 210 | 95 PS | 69 kW |
| TBO | 2.000 h/ 12 years | |
mt-propeller 2-blade constant-speed MTV-21-A/175-05, TBO 2.000 h/ 6 years
ЛТХ
| Max. speed | 165 kts | 190 mph | ||
|---|---|---|---|---|
| Max. level speed, MSL | 130 kts | 150 mph | ||
| 75%, 5,000 ft, ISA | 55%, 5,000 ft, ISA | |||
| Speed (TAS) | 121 kts | 140 mph | 103 kts | 118 mph |
| Range (+ 45 min rsv) | 535 NM | 990 km | 620 NM | 1,150 km |
| Endurance (+ 45 min rsv) | 4:30 hrs | 6:05 hrs | ||
| Fuel-flow | 21.5 ltr/h | 5.7 gph | 16.6 ltr/h | 4.36 gph |
| Stallspeed clean VS1 | 50 ks | 58 mph | ||
| Stallspeed in landing configuration VS0 |
43 kts | 50 mph | ||
| Max. demonstrated crosswind | 15 kts | 3.8 m/s | ||
| Rate of climb, sea level | 750 ft/min | 3,8 m/s | ||
| Service ceiling | 14,500 ft | 4,450 m | ||
| Empty weight, typical | 500 kg | 1,103 lb |
|---|---|---|
| Max. takeoff weight | 750 kg | 1,654 lb |
| Useful load (at standard equipment) | 250 kg | 551 lb |
| Max. baggage weight | 40 kg | 97 lb |
| Max. wing loading | 71.5 kg/m² | 16.6 lb/sqft |
| Seats | 2 | |
| Fuel capacity 100LL or Eurosuper 95 |
2 x 60 ltr | 2 x 16 gal (US) |
| Takeoff distance, ground roll | 250 m | 820 ft |
|---|---|---|
| Takeoff distance over 50 ft obstacle |
470 m | 1,540 ft |
| Landing distance, ground roll | 200 m | 650 ft |
| Landing distance over 50 ft obstacle |
500 m | 1.640 ft |
Проспект с описанием самолета
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