Aquila A 211

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

A 211
Role Light 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

References
Wikimedia Commons has media related to Aquila A 211.
  1. "Aquila Aviation". Retrieved 25 August 2013.
  2. "Aquila debuts in U.S." Archived from the original on 1 February 2014. Retrieved 25 August 2013.
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