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Specification

AQUILA A212 TURBO

The AQUILA A212 Turbo is a single-engine high performance with turbocharger 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 G3X)

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.

4 A212 Turbo aircraft in our fleet.

TC-UGO / TC-UDO / TC-UHL / TC-UIN

TECHNICAL SPECIFICATIONS

ENGINE

Bombardier Rotax 914 F3

POWER

115 HP

PROPELLER

MT Propeller 2 Blade Constant Speed

AVIONICS

Flight Instruments

Garmin G3X

Engine Instruments

MVP-50P

GPS

GARMIN GTN650

PERFORMANCE

Max Speed

165 kts

Cruise Speed

130kt (%75 Power)

Range

620NM (%55 Power)

Endurance (+45 min reserve)

6:05 saat (%55 Power)

Service Ceiling

14.500ft

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

250 m / 445 m

Landing Distance (Ground Roll / Over 50ft)

230 m / 510 m

WEIGHT AND CAPACITY

Empty Weight

530 kg

Useful Load

270 kg

Maximum Take-off Weight

800 kg

Fuel Capacity

2 x 60 ltr

 

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