Quander has built a simple structure as a low power single seater. The wing is normally a Vento 13 sq.m.

Empty weight: 68 kg
Wing span: 9.5 m
Wing area: 13 sq.m
Fuel capacity: 20 lt
Certification: vVz
Engine: Hirth F33, 25 hp
MAUW: 300 kg
Seats: 1
Max speed: 90 kph
Cruise speed: 65-75 kph
Minimum speed: 42 kph
Climb rate: 3.1 m/s
Fuel consumption: 4.3 lt/hr
Price (1998): 17 40 DM

A very old but very rigid double-pole design, usually flown with a 13 sq.m Vento wing.

The Quander Airpfeil (English: Air-Arrow) is a German ultralight trike that was designed and produced by UL Flugzeugbau Quander of Petershagen. The aircraft is supplied complete and ready to fly.

Empty weight: 130 kg
Wing span: 9.5 m
Wing area: 13 sq.m
Fuel capacity: 62 lt
Certification: Vz
Engine: Rotax 582, 65 hp
MAUW: 400 kg
Seats: 2
Max speed: 145 kph
Cruise speed: 80-120 kph
Minimum speed: 43 kph
Climb rate: 5.4 m/s
Fuel consumption: 10 lt/hr
Price (1998): 38 400 DM

2009 Price: 15000 EURO

Tomi Cross 5,1 / MW 155 VingeTrike
Stall: 50 kt / 58 mph / 93 kmh
Cruise: 83 kt / 95 mph / 153 kmh
VNE: 100 kt / 115 mph / 185 kmh
Empty Weight: 204 kg / 450 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 300 ft/min / 2 m/s
Glide Ratio: 1:8
Take-off distance (50ft obstacle): 610 ft / 185 m
Landing distance (50ft obstacle): 850 ft / 260 m

Tennessee Propellers of Normandy, Tennessee, is a company better known for their wooden maple laminate aircraft propellers, but the company also acted as the exclusive distributor for the Zenoah G-25 and G-50 line of engines. To compliment these product lines they developed the Scout powered parachute which is powered by the 45 hp (34 kW) G-50 driving a Tennessee propeller.

The Scout was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category’s maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 225 lb (102 kg). It features a parachute-style high-wing, single-place accommodation, tricycle landing gear and a single G-50 engine in pusher configuration. The 50 hp (37 kW) Rotax 503 engine was a factory option.

The aircraft carriage is built from powder coated welded 6061-T6 aluminum tubing and is a highly simplified design compared to other powered parachutes. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the same foot pedals control the nosewheel steering. The main landing gear incorporates fiberglass spring rod suspension. Standard equipment factory provided included a large canopy-stowage bag, electric engine starting, flight instruments and a four-point pilot harness.

The Scout was supplied as a complete ready-to-fly aircraft, introduced in 1999, but is no longer available. Unit cost in 2001 was US$10,000.

Engine: 1 × Zenoah G-50, 45 hp (34 kW)
Wing area: 400 sq ft (37 sq.m)
Empty weight: 225 lb (102 kg)
Gross weight: 485 lb (220 kg)
Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
Cruise speed: 25 mph (40 km/h; 22 kn)
Rate of climb: 400 ft/min (2.0 m/s)
Wing loading: 1.21 lb/sq ft (5.9 kg/sq.m)
Crew: one