Foxcon Terrier 200

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.

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.

Variants

Terrier 200

Base model with two molded individual seats.

Terrier 200C

Model with bench seats that fold into a 200 by 105 cm (79 by 41 in) bed for camping.

Specifications (Terrier 200)

Data from Bayerl and Foxcon

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: 222 km/h; 138 mph (120 kn)

Cruise speed: 204 km/h; 127 mph (110 kn)

Stall speed: 70 km/h; 44 mph (38 kn)

Never exceed speed: 241 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)