Aquila A 211

Design and development

The A 211 is the follow on to the A 210. The A 211 is a low wing, side by side seating, single engine aircraft with tricycle landing gear. The aircraft is certified under German/EASA Part 21.17 rules. The A 211 is similar to the Aquila A 210 but has a revised spinner, cowling and canopy.

Variants

Aquila A 210

Earlier model

Aquila A 211

Conventional instrument panel

Aquila A 211GX

Glass cockpit model

Specifications (A 211)

Data from Manufacturer

General characteristics

Crew: 1

Capacity: 1

Length: 7.4 m (24 ft 3 in)

Wingspan: 10.3 m (33 ft 10 in)

Height: 2.4 m (7 ft 10 in)

Wing area: 10.5 m² (113 sq ft)

Empty weight: 520 kg (1,146 lb)

Max takeoff weight: 750 kg (1,653 lb)

Fuel capacity: 120 litres (26 imp gal; 32 US gal)

Powerplant: 1 × Rotax 912S horizontally opposed piston aircraft engine, 73.5 kW (98.6 hp)

Propellers: 2-bladed MT-Propeller constant-speed MTV-21-A/175-05

Performance

Maximum speed: 266 km/h; 143 kn (165 mph)

Cruise speed: 209 km/h; 113 kn (130 mph)

Range: 990 km (615 mi; 535 nmi)

Service ceiling: 4,400 m (14,500 ft)

Rate of climb: 3.8 m/s (750 ft/min)

Wing loading: 81 kg/m² (16.6 lb/sq ft)