The Aquila A 211 is a German, two seat side-by-side configuration light aircraft, built by Aquila Aviation.

A 211
Role	Light aircraft Type of aircraft
National origin	Germany
Manufacturer	Aquila Aviation
First flight	2000
Developed from	Aquila A 210

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.[1] 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.[2]

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: one
• Capacity: one passenger
• 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 (165 mph, 143 kn)
• Cruise speed: 210 km/h (130 mph, 110 kn)
• Range: 990 km (620 mi, 530 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)

See also

Related development

• Aquila A 210

References

Wikimedia Commons has media related to Aquila A 211.