Redfern DH-2

Engine: Kinner B5, 125 hp
HP range: 125-150
Height: 9.5 ft
Length: 25.21 ft
Wing span: 28.25 ft
Wing area: 266 sq.ft
Fuel cap: 30 USG
Weight empty: 1081 lb
Gross: 1441 lb
Speed max: 93 mph
Cruise: 75 mph
Range: 275 sm
Stall: 45 mph
ROC: 700 fpm
Take-off dist: 75 ft
Landing dist: 300 ft
Service ceiling: 14,000 ft
Seats: 1
Landing gear: tail wheel

Raven 2XS

Introduced in 2009, the Raven 2XS (English: To Excess) is a Canadian aerobatic amateur-built biplane, designed and produced by Raven Aircraft of Surrey, British Columbia. The aircraft is supplied as a kit or as plans for amateur construction.

Developed from the Pitts Special, the 2XS features a strut-braced biplane layout, a two-seats-in-tandem enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration. The cockpit is 24 in (61 cm) wide.

The aircraft is made from mixed construction, using welded steel tubing, aluminum and wood, with its flying surfaces covered in doped aircraft fabric. Construction time from the supplied kit is estimated as 2000 hours.

By November 2012 one example had been registered in the United States with the Federal Aviation Administration, but none in its home country with Transport Canada. Unit cost: US$24,000 (kit only, less engine, instruments, 2011)

Engine: 1 × Lycoming IO-540, 280 hp (210 kW)
HP range: 260-400
Propellers: 3-bladed composite
Length: 19 ft 4 in (5.89 m)
Wingspan: 19 ft 2 in (5.84 m)
Height: 6 ft 6 in (1.98 m)
Wing area: 119.4 sq ft (11.09 m2)
Empty weight: 1,180 lb (535 kg)
Gross weight: 1,780 lb (807 kg)
Fuel capacity: 37 U.S. gallons (140 L; 31 imp gal)
Maximum speed: 200 mph (322 km/h; 174 kn)
Cruise speed: 188 mph (163 kn; 303 km/h)
Stall speed: 60 mph (52 kn; 97 km/h)
Range: 450 mi (391 nmi; 724 km)
Rate of climb: 3,300 ft/min (17 m/s)
Wing loading: 14.9 lb/sq ft (73 kg/m2)
Roll rate: 330 degrees/second.
Takeoff dist: 530 ft
Landing dist: 750 ft
Seats: 2 tandem
Cockpit width: 24 in
Landing gear: tailwheel

RagWing RW26 Special II

Qualifies as an LSA. The “Special II” can be built as a legal ultralight trainer or with a larger engine, as an experimental. The “Special II” basic kit will be an all-wood kit, like the single seat, to keep the pricing affordable. These kits are fairly fast to build. The kit was planned to be available in a steel tube version.

Engine: Rotax 503, 52 hp
HP range: 52-100
Length: 18 ft
Wing span: 18 ft
Wing area: 120 sq.ft
Fuel capacity: 14 USG
Empty weight: 450 lb
Gross weight: 950 lb
Cruise: 85 mph
Stall: 38 mph
Range: 350 sm
Rate of climb: 800 fpm
Takeoff dist: 350 ft
Landing dist: 450 ft
Seats: 2 tandem
Cockpit width: 24 in
Landing gear: tail wheel

Engine: 1835cc VW 60 hp
Span: 28′
Length: 15′
Empty Weight: 275 lbs
Useful Load: 250 lbs
Wing Area: 120 sq ft
Seats: 1
Take Off Distance: 200 ft
Stall: 32 mph
Landing Speed: 42 mph
Cruise: 85 mph
Rate of Climb: 750 fpm