SPECIFICATIONS & PERFORMANCE

ENGINE

Bombardier Rotax 912S
Cylinders4
Rated power100 PS73,5 kW
Max. take off power and max. continuous power A 21095 PS69 kW
TBO2.000 h15 years

PROPELLER

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

PERFORMANCE

Max. speed165 kts190 mph
Max. level speed, MSL130 kts150 mph
75%
5.000 ft
ISA
55%
5.000 ft
ISA
Speed (TAS)121 kts140 mph103 kts118 mph
Range (+ 45 min rsv)535 NM990 km620 NM1,150 km
Endurance (+ 45 min rsv)4:30 hrs6:05 hrs
Fuel-flow21,5 ltr/h5.7 gph16,6 ltr/h4.36 gph
Stallspeed clean VS149 kts58 mph
Stallspeed in landing
configuration VS0
39 kts50 mph
Max. demonstrated crosswind15 kts17 mph
Rate of climb, sea level750 ft/min3.8 m/s
Service ceiling14.500 ft4.450 m

WEIGHTS & CAPACITIES

Empty weight, typicalab 500 kgfrom 1,102 lb
Max. takeoff weight750 kg1,654 lb
Useful load (at standard equipment)250 kg551 lb
Max. baggage weight40 kg97 lb
Max. wing loading71.5 kg/m²16.6 lb/sqft
Seats2
Fuel capacity
100LL or Eurosuper 95
2 x 60 ltr2 x 16 gal (US)

TAKEOFF & LANDING DISTANCES

Takeoff distance, ground roll250 m820 ft
Takeoff distance over 50 ft
obstacle
430 m1,540 ft
Landing distance, ground roll200 m650 ft
Landing distance over 50 ft
obstacle
500 m1,640 ft

FACT SHEET
Fact sheet AQUILA A211