The Skyseeker Explorer bears a passing resemblance to the Worldwide Clipper, except that the company has stuck to aluminum tubing for the fuselage instead of the Clipper’s welded steel. Powered by a Rotax 277.
Engine: Rotax 277
Max speed: 75 mph
The Skyseeker Explorer bears a passing resemblance to the Worldwide Clipper, except that the company has stuck to aluminum tubing for the fuselage instead of the Clipper’s welded steel. Powered by a Rotax 277.
Engine: Rotax 277
Max speed: 75 mph

Empty wt: 252 lbs
Wing span: 32 ft
Wing area: 160 sq.ft
Height: 9 ft 9 in
Length: 19 ft
Fuel cap; 5 USG
Construction: Aluminium, Dacron
Engine: Rotax 277 (268 cc) 28 hp
Static thrust: 180 lbs
Max wt: 496 lbs
Stall: 20 mph
Max speed: 60 mph
Vne: 75 mph
Climb rate: 750 fpm @ 30 mph
Design limit: +4, -2g
Glide ratio: 6-1
Wing loading: 3.1 lbs/sq.ft
Power loading: 17.71 lbs/hp
1984: PO Box 243, Dept. GR, 101 Brady Rd, Winnipeg, Manitoba, Canada R3V 1L6.
UL builder
The Skyriders company builds a European version of the Ultralight Flight Phantom, which is identical to the American machine except for the power pack and a larger fuel tank.
Ultralight Flight fit a Kawasaki TA440 engine and, while this variant remains avail¬able in Europe, the popularity of Robin engines in Europe has led Skyriders to standardise on the Robin EC44 power unit.
Nicklow En¬gineering supplies his engine in lightweight form, without cooling fan, in which guise it gives 295 lb (134 kg) of static thrust.
Engine: Robin EC44, 58 hp at 7200 rpm
Propeller diameter and pitch 60 x 30 inch 1.52 x 0.76 m
Toothed belt reduction, ratio 2.5/1
Max static thrust 295 lb, 134 kg
Power per unit area 0.41 hp/sq.ft, 4.4 hp/sq.m
Fuel capacity 6.0 US gal, 5.0 Imp gal, 22.7 litre
Empty weight 229 lb, 104kg
Max take off weight 509 lb, 231 kg
Payload 280 lb, 127 kg
Max wing loading 3.61 lb/sq.ft, 17.6 kg/sq.m
Max power loading 8.8 lb/hp, 4.0kg/hp
Max recommended level speed 70mph, 113kph
Max possible level flight speed >80mph, >129kph
Never exceed speed 100 mph, 161 kph
Max cruising speed 70mph, 113kph
Economic cruising speed 50 mph, 80 kph
Stalling speed 28 mph, 45 kph
Max climb rate at sea level 1500 ft/ min, 7.6 m/s
Take off distance 60 ft, 18 m on concrete
Landing distance 50 ft, 15 m on concrete
Range at average cruising speed 150 mile, 241 km
1982: Quenchurst Ltd t/a Skyriders, Halesfield 19, Telford, Shropshire TF7 4QT, Great Britain.
UL builder

Manufactured by Skyreach Aircraft of Johannesburg, South Africa, the aircraft construction is tubular Aluminium with anodised Stainless steel joiners, composite cowlings and Trylam wing and Fuselage coverings with Rip Block.

Known previously as the Cheetah, the BushCat tube/dacron sailcloth envelope, ultralight-style S-LSA had a $49,995 base price. By 2019 that was $113000.

Good short field take-off and landing capabilities a 90kt cruise.

Rotax 582, 65HP
Empty Weight: 617 lb
Wing Span: 31,5ft
Wing Area: 142 sq.ft
Wing Chord: 54 in
Aircraft length: 18,6 ft
Aircraft Height: 6,63 ft
Cabin Height: 54 in
Cabin Width: 47,25 in
Baggage Compartment: 2 x 25 L (81 lbs max)
Fuel Capacity: 24,8 gallons
Propeller (Recommended): 3 Blade Kiev
Fuel Consumption (80% power): 3,8 gal/hour
Take Off Roll: 328 ft
Rate of Climb: 700 ft/min
Service Ceiling: 12 000 ft
Max Crosswind Component: 32 MPH
Cruise Speed (65%): 75 MPH
VNE: 125 MPH
Glide Ratio: 10-1
Power Off Stall (no flaps): 40 MPH
Power Off Stall (with flaps): 35 MPH
Landing Ground Roll: 235 ft
Gross Weight: 1245 lb
Useful Load: 628 lbs
Load Factors: + 6/- 4
Endurance (with reserves): 6,5 hrs
Range (with reserves): 500 Miles
Rotax 912UL, 80HP
Empty Weight: 617 lb
Wing Span: 31,5ft
Wing Area: 142 sq.ft
Wing Chord: 54 in
Aircraft length: 18,6 ft
Aircraft Height: 6,63 ft
Cabin Height: 54 in
Cabin Width: 47,25 in
Baggage Compartment: 2 x 25 L (81 lbs max)
Fuel Capacity: 24,8 gallons
Propeller (Recommended): 3 Blade Kiev
Fuel Consumption (80% power): 4,5 gal/hour
Take Off Roll: 292 ft
Rate of Climb: 1000 ft/min
Service Ceiling: 12 000 ft
Max Crosswind Component: 32 MPH
Cruise Speed (65%): 95 MPH
VNE: 125 MPH
Glide Ratio: 10-1
Power Off Stall (no flaps): 40 MPH
Power Off Stall (with flaps): 35 MPH
Landing Ground Roll: 235 ft
Gross Weight: 1245 lb
Useful Load: 628 lbs
Load Factors: + 6/- 4
Endurance (with reserves): 7,5 hrs
Range (with reserves): 600 Miles
Rotax 912ULS, 100HP
Empty Weight: 617 lb
Wing Span: 31,5ft
Wing Area: 142 sq.ft
Wing Chord: 54 in
Aircraft length: 18,6 ft
Aircraft Height: 6,63 ft
Cabin Height: 54 in
Cabin Width: 47,25 in
Baggage Compartment: 2 x 25 L (81 lbs max)
Fuel Capacity: 24,8 gallons
Propeller (Recommended): 3 Blade Kiev
Fuel Consumption (80% power): 5 gal/hour
Take Off Roll: 262 ft
Rate of Climb: 1200 ft/min
Service Ceiling: 14 000 ft
Max Crosswind Component 32 MPH
Cruise Speed (65%): 105 MPH
VNE: 125 MPH
Glide Ratio: 10-1
Power Off Stall (no flaps): 40 MPH
Power Off Stall (with flaps): 35 MPH
Landing Ground Roll: 235 ft
Gross Weight: 1245 lb
Useful Load: 628 lbs
Load Factors: + 6/- 4
Endurance (with reserves): 7,0 hrs
Range (with reserves): 700 Miles
Amphibian 912ULS, 100HP
Empty Weight: 865 lb
Wing Span: 31,5ft
Wing Area: 142 sq.ft
Wing Chord: 54 in
Aircraft length: 18,6 ft
Aircraft Height: 8,10 ft
Cabin Height: 54 in
Cabin Width: 47,25 in
Baggage Compartment: 2 x 25 L (81 lbs max)
Fuel Capacity: 24,8 gallons
Propeller (Recommended): 3 Blade Kiev
Fuel Consumption (80% power): 5 gal/hour
Take Off Roll: 540 ft (water)
Rate of Climb: 850 ft/min
Service Ceiling: 12 000 ft
Max Crosswind Component: 20 MPH
Cruise Speed (65%): 90 MPH
VNE: 115 MPH
Glide Ratio: 8-1
Power Off Stall (no flaps): 40 MPH
Power Off Stall (with flaps): 35 MPH
Landing Ground Roll: 305 ft
Gross Weight: 1430 lb
Useful Load: 565 lb
Load Factors: + 4/- 2
Endurance (with reserves): 7,0 hrs
Range (with reserves): 650 Miles

An LSA kit plane.
Cruise: 105 mph
Stall: 36 mph
Range: 460 sm
Rate of climb: 1200 fpm
Takeoff dist: 125 ft
Landing dist: 500 ft
Engine: Rotax 912, 80 hp
HP range: 50-100
Fuel capacity: 20 USG
Empty weight: 575 lb
Gross weight: 1212 lb
Length: 18.6 ft
Wing span: 31 ft
Wing area: 162 sq.ft
Seats: 2
Cockpit width: 43 in
Landing gear: nosewheel

The Frontier side by side is a bush plane kit aircraft. The Frontier Kit is divided into three sub-kits. Each sub kit comes with everything needed to finish the job. Complete, step-by-step instructions with illustrations and photos are included with each kit. The complete airframe should be ready to cover in only a few days.
The fuselage kit includes a powder coated fuselage that is ready to attach parts to. The builder will install the rudder pedals, master cylinders and pulleys. When the fuel system and control cables are installed the fuselage will be ready be covered.
The standard fuselage kit sold for US$16,200 in 2009.
The wing kit includes everything needed to finish the wings, flaps, ailerons, fuel tanks, and fabric system. Every nut and washer, screw and component part is in the kit. Attaching pulleys, running cables and urethaning ribs is all that is necessary prior to covering.
The standard wing kit sold for US$8,800 in 2009.
The finishing kit includes everything that doesn’t come in the first two kits, minus paint, the instruments, and the FWF. It includes: the engine cowl, engine mount, windows, seats with standard upholstery, shoulder harnesses and seat belts, boot cowl assembly and firewall, instrument panel, landing gear system, tailwheel and tail spring, 8:00 x 6 tires and tubes, and wing struts.
The standard finishing kit sold for US$7,600 in 2009.
Sky Raider Frontier
Lycoming 290
Gross Weight 1320/1600 Ibs
VNE 130 mph
Wing span wlo wing tips 30 ft
Cruise 105 mph
Wing Area wi wing tips 107 sq. ft
Stall w/ Flaps 40 deg 38 mph
Length 22 ft 2 in
Stall clean 42 mph
Height 6 ft 8 in
Take off Roll 250 ft
Width Folded 7 ft 9 in
Climb Rate 820 fpm
Length Folded 22 ft 2 in
Empty weight 916 lbs
Gear Width 76 in
Useful load 682 lbs
Cabin Width 47 in
Load limit factors +6g – 4g
Fuel Capacity 26 USgal

Sky-MAXX gives higher cruise speeds with aircraft in the Light Sports Aircraft (LSA/SLA) or microlight/ultralight category. Of full aluminium construction, Sky-MAXX is a conventional, three axis, non-strut-braced monoplane. It’s high lift wing, incorporating electrical flaps, produces short take-off and landing (STOL) performance, whilst maintaining a 180 km/h cruise. The two seat Sky-MAXX was designed with an all-metal duralumin alloy structure.
Several editions (tropical, desert, photography) “Ready for fly” or as a kit. 2009 Price: US$ 95,000 / EUR 80,750
Engine: Rotax 80-102 hp, HIRTH, BMW, Jabiru 6-cylinder
Empty Weight: 270 kg / 595 lbs
MTOW Weight: 750 kg / 1653 lbs
Stall: 35 kt / 40 mph / 65 kmh
Cruise: 108 kt / 124 mph / 200 kmh
VNE: 139 kt / 160 mph / 258 kmh
Climb Rate: 1400 ft/min / 7 m/s
Take-off distance (50ft obstacle): 100 ft / 30 m
Landing distance (50ft obstacle): 100 ft / 30 m

LSA variations on the Carlson Aircraft Sparrow.
Sparrow Sport Special
Cruise: 85 mph
Stall: 31 mph
Range: 350 sm
Rate of climb: 1750 fpm
Takeoff dist: 85 ft
Landing dist: 175 ft
Engine: Rotax 503, 52 hp
HP range: 50-68
Fuel capacity: 10 USG
Empty weight: 400 lb
Gross weight: 775 lb
Length: 16.8 ft
Wing span: 26 ft
Wing area: 117 sq.ft
Seats: 1
Cockpit width: 24 in
Landing gear: tailwheel
Sparrow II XTC
Cruise: 110 mph
Stall: 39 mph
Range: 460 sm
Rate of climb: 1100 fpm
Takeoff dist: 250 ft
Landing dist: 350 ft
Engine: Rotax 912, 80 hp
HP range: 80-100
Fuel capacity: 24 USG
Empty weight: 630 lb
Gross weight: 1300 lb
Length: 18 ft
Wing span: 31.1 ft
Wing area: 140 sq.ft
Seats: 2
Landing gear: nose or tail