Specifications / Performance

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Engine

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 2.000 h/ 15 years

Propeller

Propeller

mt-propeller 2-blade constant-speed MTV-21-A/170-05,
TBO 2.000 h/ 6 years

Performance and Airspeeds

Performance and Airspeeds

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

Weights and Capacities

Weights and Capacities

Empty weight, typical

ab 500 kg

from 1102 lb
Max. takeoff weight 750 kg 1,653 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 and Landing Distances

Takeoff and Landing Distances

Takeoff distance, ground roll 250 m 820 ft
Takeoff distance over 50 ft
obstacle
430 m 1,411 ft
Landing distance, ground roll 200 m 650 ft
Landing distance over 50 ft
obstacle
500 m 1.640 ft

These information are also available as PDF file for download:

AQUILA A211 - Specifications and Performance (1.1 MB)

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News and Updates

24.03.17

AQUILA Aviation is featured at this year's AERO at Friedrichshafen with newest highlights and...

09.01.17

We have been waiting for quite a while, but finally we received them: the new scalemodel of our...

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