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Specification

AQUILA A211

The AQUILA A211 is a single-engine airplane in composite construction and designed for cruising and training.

It is equipped with two side-by-side seats, low wings and a cruciform tail. The spacious, enclosed cockpit provides sufficient room even for tall pilots. Complete glazing of the canopy allows an excellent all-round vision.

Baggage compartment capacity and loading is meeting even the highest demands. Low fuel consumption and a high cruising speed allow a range that is exceptional in this category of aircraft.

2 A211 aircraft in our fleet

TC-UBL / TC-UCL

TECHNICAL SPECIFICATIONS

ENGINE

Bombardier Rotax 912S

POWER

100 HP

PROPELLER

MT Propeller 2 Blade Constant Speed

AVIONICS

Flight Instruments

Garmin G5

Engine Instruments

Analog

GPS

Garmin GNS650

PERFORMANCE

Max Speed

165 kts

Cruise Speed

121kt (%75 Power) – 103kts (%55 Power)

Range

620NM (%55 Power)

Endurance (+45 min reserve)

6:05 saat (%55 Power)

Stall Speed (Vs1)

49kts

Stall Speed (Vs0)

39kts

Cross Wind Limitation

15kts

Service Ceiling

14.500ft

Take-off Distance (Ground Roll / Over 50ft)

250 m / 430 m

Landing Distance (Ground Roll / Over 50ft)

200 m / 500 m

WEIGHT AND CAPACITY

Empty Weight

500 kg

Useful Load

250 kg

Maksimum Take-off Weight

750 kg

Fuel Capacity

2 x 60 ltr

 

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