A 210

Aquila Technische Entwicklungen GmbH

Приборная доска:

фотографии с сайта www.aquila-aero.com

Engine
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 1.500 hrs

Propeller
mt-propeller 2-blade constant-speed MTV-21-A/175-05

Performance and airspeeds
Max. speed 190 mph
Max. level speed, MSL 150 mph
 
Speed (TAS) 140 mph
Range (+ 45 min rsv) 990 km
Endurance (+ 45 min rsv) 4:30 hrs
Fuel-flow 21.5 ltr/h
     
Stallspeed clean VS1 58 mph
Stallspeed in landing
configuration VS0 50 mph
Max. demonstrated crosswind 3.8 m/s
Rate of climb, sea level 3,8 m/s
Service ceiling 4,450 m

Weights and capacities
Empty weight, typical 500 kg
Max. takeoff weight 750 kg
Useful load 250 kg
Max. baggage weight 40 kg
Max. wing loading 71.5 kg/m²
Seats 2
Fuel capacity
100LL or Eurosuper 95 2 x 60 ltr

Takeoff and landing distances
Takeoff distance, ground roll 250 m
Takeoff distance over 50 ft
obstacle 470 m
Landing distance, ground roll 200 m
Landing distance over 50 ft
obstacle 500 m

Сайт разработчика: www.aquila-aero.com