Aquila A 211
| A 211 | |
|---|---|
 | |
| Role | Light aircraft |
| National origin | Germany |
| Manufacturer | Aquila Aviation |
| Developed from | Aquila A 210 |
The Aquila A 211 is a German, two seat side-by-side configuration light aircraft, built by Aquila Aviation.
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: 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: 4,420 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. |
- ↑ "Aquila Aviation". Retrieved 25 August 2013.
- ↑ "Aquila debuts in U.S.". Retrieved 25 August 2013.
This article is issued from Wikipedia - version of the 9/16/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.