Engineering:Foxcon Terrier 200
| Terrier 200 | |
|---|---|
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| |
| Foxcon Terrier 200C | |
| Role | Light-sport aircraft |
| National origin | Australia |
| Manufacturer | Foxcon Aviation |
| Status | In production |
The Foxcon Terrier 200 is an Australian light-sport aircraft, designed and produced by Foxcon Aviation of Mackay, Queensland. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1][2]
Design and development
The Terrier 200 was designed to comply with the US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.[1][2]
The aircraft is made from vacuum-molded composites with the design goal of strength at a light weight. Its 8.7 m (28.5 ft) span wing employs a Chris Mark 4 airfoil and mounts flaps. The standard engines available in 2012 were the 80 hp (60 kW) D-Motor LF26, the 100 hp (75 kW) Rotax 912ULS, the 100 hp (75 kW) Subaru EA 81 and the 116 hp (87 kW) Lycoming IO-233-LSA four-stroke powerplants. By 2015 only the Subaru EA 81 and Rotax 912ULS were still offered. Floats for water operations are optional.[1][2][3][4][5]
Variants
- Terrier 200
- Base model with two molded individual seats.[1][2]
- Terrier 200C
- Model with bench seats that fold into a 200 by 105 cm (79 by 41 in) bed for camping.[1][2]
Specifications (Terrier 200)
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Data from Bayerl and Foxcon[1][3]
General characteristics
- Crew: one
- Capacity: one passenger
- Length: 6.10 m (20 ft 0 in)
- Wingspan: 8.7 m (28 ft 7 in)
- Height: 2.30 m (7 ft 7 in)
- Airfoil: Chris Mark 4
- Empty weight: 340 kg (750 lb)
- Gross weight: 600 kg (1,323 lb)
- Fuel capacity: 88 litres (19 imp gal; 23 US gal)
- Powerplant: 1 × Subaru EA 81 four cylinder, liquid-cooled, four stroke automotive engine, 75 kW (101 hp)
Performance
- Maximum speed: 220 km/h (140 mph, 120 kn)
- Cruise speed: 200 km/h (130 mph, 110 kn)
- Stall speed: 70 km/h (44 mph, 38 kn)
- Never exceed speed: 240 km/h (150 mph, 130 kn)
- Endurance: 6 hours
- g limits: +6/-4
- Maximum glide ratio: 12:1
- Rate of climb: 7.5 m/s (1,480 ft/min)
References
- ↑ 1.0 1.1 1.2 1.3 1.4 1.5 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 55. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ 2.0 2.1 2.2 2.3 2.4 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 56. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- ↑ 3.0 3.1 Foxcon Aviation (n.d.). "Terrier 200". http://www.foxcon.com/Specifications.html. Retrieved 10 July 2012.
- ↑ Foxcon Aviation (n.d.). "Engine Choices". Archived from the original on 4 June 2012. https://web.archive.org/web/20120604234554/http://www.foxcon.com/Engine-Choices.html. Retrieved 5 January 2015.
- ↑ Foxcon Aviation (n.d.). "Powerplants". http://www.foxcon.com/Powerplants.html. Retrieved 5 January 2015.
External links
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