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The Quad City Challenger is a family of one and two seats-in-tandem, pusher configuration, tricycle landing gear ultralight aircraft that is designed and produced by Quad City Aircraft Corporation of Moline, Illinois. The Challenger was first introduced in 1983.
The Excalibur was designed as "clone" [1] of the Quad City Challenger II aircraft. The company took the basic Challenger design and incorporated many changes, including mounting the engine upright allowing larger propellers and the Rotax gearbox to be mounted, lengthening the tailboom and enlarging the tail vertical surface to increase stability, shortening the ailerons and replacing control ...
Rotax 582 pusher installation on a Quad City Challenger II: Type Piston aero-engine: National origin: Austria Manufacturer Rotax: Major applications: Quad City Challenger Blue Yonder Merlin: Status Production to be completed by end of 2021 [1] Produced 1989-2021 [1] [2] Number built: more than 30,000 (July 2021) [1]
An aircraft type-club fly-in: A line-up of Quad City Challenger II ultralight aircraft at the annual International Challenger Owners Association Ski Fly-in at Montebello Quebec, 29 January 2005. Pipers line-up at the annual convention of the Short Wing Piper Club.
The basic ultralight Ultraflight Lazair is the most produced Canadian-designed aircraft of any category. Blue Yonder Merlin EZ Canadian-designed and built advanced ultralight airplane A common advanced ultralight seen in Canada: Quad City Challenger II Jabiru Calypso 3300 advanced ultralight aircraft on amphibious floats at the Canadian Aviation Expo Fly camping at a remote aerodrome with a ...
Challenger II may refer to: Challenger 2, British main battle tank; Quad City Challenger II, ultralight aircraft; Challenger II, a microcomputer manufactured by Ohio Scientific in 1977; Challenger II, the American registration name for racehorse and leading sire Challenger (horse)
Parts books were often issued as microfiche, though this has fallen out of favour. Now, many manufacturers offer this information digitally in an electronic parts catalogue. This can be locally installed software, or a centrally hosted web application. Usually, an electronic parts catalogue enables the user to virtually disassemble the product ...
Data from Rans website General characteristics Crew: one Capacity: one passenger Length: 21 ft 8 in (6.60 m) Wingspan: 31 ft 0 in (9.45 m) Height: 7 ft 4 in (2.24 m) Wing area: 152 sq ft (14.1 m 2) Aspect ratio: 6.33:1 Empty weight: 475 lb (215 kg) Gross weight: 975 lb (442 kg) Fuel capacity: 18 US gallons (68 litres) Powerplant: 1 × Rotax 582, 64 hp (48 kW) Propellers: 2-bladed wooden, 5 ft ...
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