Designed to meet the FAR Part 103 requirements.
Engine: Rotax 447, 40 hp
HP range: 35-40
Top speed: 63 mph
Cruise: 50 mph
Stall: 28 mph
Range: 120 nm
Rate of climb: 800 fpm
Takeoff dist: 175 ft
Landing dist: 175 ft
Service ceiling: 8000 ft
Fuel capacity: 5 USG
Empty weight: 250 lb
Gross weight: 485 lb
Length: 16 ft
Wing span: 24 ft
Wing area: 145 sq.ft
Seats: 1
Undercarriage: tailwheel
Engine: Zenoah, 22 hp
HP range: 12-22
Cruise: 30 mph
Stall: 18 mph
Rate of climb: 250 fpm
Takeoff dist: 75 ft
Landing dist: 50 ft
Fuel capacity: 3 USG
Empty weight: 145 lb
Gross weight: 345 lb
Length: 17.5 ft
Wing span: 32 ft
Wing area: 157 sq.ft
Seats: 1
Cockpit width: 26 in
Landing gear: tailwheel
LSA: yes
2001: 74 Brookwood Dr, Marietta, GA 30064, USA.
UL plans supplier
All Viking 130 engines use Variable Valve timing and Variable Valve Lift. The 130 is as close to a Honda Fit car engine as possible, retaining all of its modern features.
The Honda based Viking engine technology include 100% liquid cooling, computerized engine management, networked engine monitor capability, digital ECU, variable intake cam timing, gasoline direct injection fuel system and variable intake valve lift.
The engines are Evans liquid cooled without pressure and run at only 2/3 Honda rated RPM redline. Only one wire and a fuel pump to connect for start. Direct injected, no complicated fuel return system needed.
The 2016 Honda Fit engine manual cover all engine specifics. Cowlings, engine mounts and propeller available along with all other accessories. The Viking has no external exhaust pipes, just a muffler.
The engines are ready to bolt to the airframe as shipped
Designed by Jan Eggenfellner, the Viking 110 is a 110hp aircraft engine developed from Honda Fit engine components by Viking Aircraft Engines.
Applications:
Zenith CH-601 CH-650 CH-701 CH-750
Van’s RV-12
Sonex Aircraft Sonex
Just Highlander
Progressive Aerodyne SeaRey
Viking 110
Type: Inline 4 cylinder
Bore: 73mm
Stroke: 90mm
Displacement: 1497cc
Length: 24.64in
Width: 22in
Height: 21.32in
Dry weight: 178lb
Cooling system: liquid
Reduction gear: 2.33/1
Power output: 110hp
Compression ratio: 10.4
Fuel consumption: 8.5gph max
Designed by Robert J. Walters and winner of the Outstanding New Design Award at Oshkosh 1980, the Dragonfly is another canard-configured composite homebuilt in the same vein as the Quickie and VariEze. First flying on 16 June 1980 (N5WN) with two-place side-by-side seating under a bubble canopy, the Dragonfly is powered by a 56 hp 1600cc HAPI/VW engine. The intention of the aircraft is to provide builders with a project that is inexpensive to build and also inexpensive to operate on a readily available engine. The wing and canard are built as a single piece in a jig and the job can be accomplished in a normal two-car garage. The cockpit width is 43 inches, like that of a Cessna 172. A molded canopy was selected to avoid the soapbubble effect of a free-blown canopy. A typical 140-mph cruise burns gas at the rate of 45 mpg. The propeller used is a Great American, with a 40-inch pitch and 52-inch diameter.
Available in three under-carriage options as Mk.I, II or III.
By 1998, out of 2000 plans or kits that had been sold, about 500 were finished.
This 2 place composite design can be built from plans or can be quick built using pre-fab parts.
The DRAGONFLY, in 2008 was available from:
DART Industries
PO Box 223, Botha’s Hill
Kwazula Natal, So Africa 3660
Engine: VW
Wing span: 6.71 m
Wing area: 9.45 sq.m
MAUW: 522 kg
Empty weight: 277 kg
Fuel capacity: 57 lt
Max speed: 290 kph
Cruise speed: 265 kph
Minimum speed: 77 kph
Climb rate: 4 m/s
Seats: 2
Plan price (1998): $260
Kit price (1998): $8600
Engine 45-hp 1600 cc Volkswagen
Gross Wt. 1075 lb
Empty Wt. 805 lb
Fuel capacity 15 USG
Wingspan 22 ft
Wing area: 97 sq.ft
Top speed 150 mph
Cruise 155 mph
Climb rate 800 fpm solo
Ceiling 17,000 ft
Seats: 2
Dragonfly
Engine 56hp 1600 cc HAPI/Volkswagen
Wingspan 22 ft
Wing area: 97 sq.ft
Length: 19’0″
Gross Wt. 1075 lb
Empty Wt. 805 lb
Fuel capacity 15 USG
Top speed 168 mph
Cruise 140 mph
Stall: 45 mph
Climb rate 1050 fpm solo
Ceiling 18,500 ft
Range: 500 mi
Seats: 2
Engine: VW 1835cc
Speed max: 180 mph
Cruise: 165 mph
Range: 550 sm
ROC: 850 fpm
Take-off dist: 1200 ft
Landing dist: 2000 ft
Service ceiling: 18,500 ft
HP range: 60-82
Fuel cap: 15 USG
Weight empty: 610 lbs
Gross: 1150 lbs
Height: 4.2 ft
Length: 20 ft
Wing span: 22 ft
Wing area: 102.7 sq.ft
Seats: 2
Landing gear: tail wheel
Dart Industries Dragonfly
Stall: 58 kt / 67 mph / 107 kmh
Cruise: 145 kt / 167 mph / 269 kmh
VNE: 200 kt / 230 mph / 370 kmh
Empty Weight: 370 kg / 815 lbs
MTOW Weight: 551 kg / 1215 lbs
Climb Ratio: 600 ft/min / 3 m/s
Engine: 2180 70HP VW
Span: 22 ft
Length: 19 ft
Empty Weight: 600 lb
Useful Load: 545 lb
Wing Area: 92.2 sq. ft.
Seats: 2 side by side
Take Off Distance: 1200 ft
Stall: 48 mph
Cruise: 165 mph
Rate of Climb: 850 fpm
1979: Viking Aircraft Ltd.
(pres: Robert J Walters),
Carlsbad CA.
USA
Offers plans and kits to construct Dragonfly two-seat composites monoplane of unusual design, with mid-mounted wings and canards, plus kits for Cygnet two-seat monoplane (originally the Sisler SF-2 Whistler).
1996-8: PO Box 646, Elkhorn, WI 53121, USA.
2008: Viking Aircraft, 333 Sunny Hill Dr, Elkhorn, Wisconsin 55312, USA
Arun Vijayan of Cochin, Kerala, India, designed and built his own microlight using galvanized and cold rolled steel pipes, mostly second hand. The engine is a converted Suzuki Samurai. Total cost was 36 000/-
Engine: Suzuki modified
Wing span: 10 m
Total Weight: 137 kg
Length: 5.93 m
Height: 2.96 m
Cochin, Kerala, India
Built an UL
Built by Vidas Navickas (Lithuania) in 2004.
NV-5 Nimfa
Stall: 32 kt / 37 mph / 60 kmh
Cruise: 54 kt / 62 mph / 100 kmh
VNE: 86 kt / 99 mph / 160 kmh
Empty Weight: 150 kg / 331 lbs
MTOW Weight: 350 kg / 772 lbs
Climb Ratio: 800 ft/min / 4 m/s
Glide Ratio: 14
Take-off distance (50ft obstacle): 390 ft / 120 m
Landing distance (50ft obstacle): 660 ft / 200 m
All Aero 