A 210 | |
---|---|
Role | Two seat light aircraft |
National origin | Germany |
Manufacturer | Aquila Aviation by Excellence |
First flight | 5 March 2000 |
Status | In production 2011 |
Primary user | Cameroon Air Force |
Number built | 120 by early 2011 |
The Aquila A 210 is a two-seat reinforced plastic light aircraft produced in Germany from 2002. It remains in production in 2022 as the updated A211.
The marketing name A 210 is usually used to refer to Aquila's light side by side two seat aircraft, though its official engineering and certification name is Aquila AT01. Design work started in 1997 and the first flight was made in March 2000. [1]
The A 210 is entirely built from carbon and glass fibre reinforced plastics (CFRP and GFRP). CRFP is used for the more highly stressed members, spars, frames and stringers, GFRP for shells and control surfaces, the latter with GFRP/polyurethane sandwich construction. The low wing has straight tapered inboard sections with increasing sweep outboard and winglets at the tips on production examples. It has a laminar flow section and 4.5° of dihedral. The ailerons are balanced and the inboard single slotted Fowler flaps have two positions. [1]
The A 210 is powered by a Rotax 912 flat four engine driving a two blade propeller. The cabin has uninterrupted transparencies fore and aft, with a slender fuselage behind. The canopy is forward hinged. The tailplane is set just above the fuselage and the fin is swept. A small ventral fin doubles as a tail bumper. The A 210 has a fixed tricycle undercarriage. Its mainwheels are fitted with hydraulic brakes and mounted on spring steel legs from the fuselage. The nosewheel has rubber suspension and is steerable; speed fairings are fitted on all wheels. [1]
German certification was achieved in 2001 and deliveries began the following year. It gained US certification in 2003. Early sales were to clubs, mostly as training aircraft. Most have been sold in Europe and overall 120 have been built by late 2010. [1] 110 appear as Aquila AT01 on the civil aircraft registrations of European countries excluding Russia in 2010. [2] [3]
Data from Jane's All the World's Aircraft 2011/12 [1]
General characteristics
Performance
Avionics
EFIS
The Tecnam P92 Echo and Tecnam P92 Eaglet are Italian high-winged, light aircraft, designed by Luigi Pascale and built by Tecnam of Naples.
The Coavio DF 2000 is a single-engine, high-wing all-metal ultralight aircraft with side-by-side seating for two. Built in Italy, production began in 2004.
The Skyeton K-10 Swift is a two-seat, single-engine light sports or ultralight aircraft designed in Ukraine.
The Dyn'Aéro MCR4S is a four-seat development of the French two seat, single engine Dyn'Aéro MCR01. It first flew in early 2000 and is sold as a kit for homebuilding in several versions by SE Aviation of Pontarlier.
The TL Ultralight TL-96 Star is a single-engine, side-by-side configuration two seat ultralight, designed in the Czech Republic in the 1990s. More than 150 have been registered.
The TL Ultralight TL-132 Condor and TL-232 Condor Plus are single engine, highwing ultralight aircraft designed and built in the Czech Republic in the mid-1990s. They remain in production in 2010.
The Roko Aero NG4 is a single-engined sport aircraft, available in both light-sport aircraft and ultralight models, which seats two side by side. It is in production in the Czech Republic.
The Eurofly FB5 Star Light is a single engine kit built Italian ultralight, seating two side by side. It first flew in the late 2000s.
The Kieger AK3 is conventionally laid out single engine, tractor configuration, low wing two seat light aircraft built in France from 2006. At least two have flown.
The Tomark Viper SD4 is a Slovak single–engine, all-metal, two-seat low wing monoplane with a fixed tricycle undercarriage and side-by-side seating for two people. The aircraft is built by Tomark s.r.o. of Prešov.
The Elitar-202 or Elitar 202 is a conventionally laid out, single engine ultralight aircraft which seats two in side-by-side configuration. Designed in Russia, production of the Type 202 began in 2003.
The UL-Jih Evolution is a conventionally laid out, two-seat, high-wing, single-engine ultralight, designed and built in the Czech Republic. Two variants were available in 2010.
The Groppo XL and Groppo Trail are very similar single engine, tandem seat, high wing ultralight aircraft designed and built in Italy. Both can be supplied complete or in kit form. The two models differ chiefly in undercarriage type.
The Scoda Aeronáutica Super Pétrel is an amphibious pusher configuration biplane, seating two side-by-side, first brought into production in Brazil in 2002 by EDRA Aeronáutica, although the original design had French parentage. Production in 2011 offered kit and flyaway forms.
The IAE VUT Marabou was built as a piloted test vehicle to develop autonomous control of unmanned aerial vehicles (UAVs) flying in civil airspace. Czech-designed and constructed, it first flew in April 2010.
The Aviakit Véga is an ultralight aircraft seating two in side-by-side configuration. It was designed in France in the late 1990s to be easily constructed by amateurs from kits and was offered with a choice of three engines and of tricycle or conventional undercarriages.
The Alpi Pioneer 400 is an Italian four-seat light aircraft, designed produced by Alpi Aviation, of Pordenone. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.
The Gidroplan Che-22 Korvet is a three-seat, parasol wing flying boat designed and built in Russia from the 1990s. It can have one or two engines and may be configured as an amphibian. At least eighty have been produced.
The Aquila A 211 is a German, two seat side-by-side configuration light aircraft, built by Aquila Aviation.
The Softeks V-24 Lastivka is a four seat, twin pusher engined utility aircraft, designed and built in Ukraine in the 2010s for survey and transport work. The first prototype flew late in 2012.