1982: Quenchurst Ltd t/a Skyriders, Halesfield 19, Telford, Shropshire TF7 4QT, Great Britain.
UL builder
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

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
Yang 28
Paraglider circa 1998.
Wing area: 28.6 sq.m
Pilot weight: 65-85 kg
No. of cells: 32
Wing span: 9.8 m
Aspect ratio: 3.4
Min sink: 1.3 m/s
Max speed: 38 kph
Yang 31
Paraglider circa 1998.
Wing area: 31 sq.m
Pilot weight: 85-105 kg
No. of cells: 34
Wing span: 10.6 m
Aspect ratio: 3.6
Min sink: 1.3 m/s
Max speed: 38 kph
Quix 26
Paraglider circa 1998.
Wing area: 26.43 sq.m
Pilot weight: 60-80 kg
No. of cells: 45
Wing span: 11.11 m
Aspect ratio: 4.67
Min sink: 1.1 m/s
Max speed: 45 kph
Quix 28
Paraglider circa 1998.
Wing area: 28 sq.m
Pilot weight: 80-95 kg
No. of cells: 45
Wing span: 11.83 m
Aspect ratio: 4.9
Min sink: 1.1 m/s
Max speed: 45 kph
Quix 31
Paraglider circa 1998.
Wing area: 31 sq.m
Pilot weight: 95-110 kg
No. of cells: 51
Wing span: 12.34 m
Aspect ratio: 4.9
Min sink: 1.1 m/s
Max speed: 45 kph
Maxi BI
Paraglider circa 1998.
Wing area: 42.3 sq.m
Pilot weight: 130-210 kg
No. of cells: 49
Wing span: 14 m
Aspect ratio: 4.6
Min sink: 1.3 m/s
Max speed: 50 kph



Divine 26R
Paraglider circa 1998.
Wing area: 26.47 sq.m
Pilot weight: 75-95 kg
No. of cells: 75
Wing span: 12.74 m
Aspect ratio: 6.13
Min sink: 0.9 m/s
Max speed: 63 kph
Divine 27
Paraglider circa 1998.
Wing area: 27.47 sq.m
Pilot weight: 75-90 kg
No. of cells: 63
Wing span: 12.13 m
Aspect ratio: 5.3
Min sink: 1 m/s
Max speed: 50 kph
Divine 29
Paraglider circa 1998.
Wing area: 29.2 sq.m
Pilot weight: 90-105 kg
No. of cells: 66
Wing span: 12.73 m
Aspect ratio: 5.55
Min sink: 1 m/s
Max speed: 50 kph
Divine 31
Paraglider circa 1998.
Wing area: 30.93 sq.m
Pilot weight: 105-120 kg
No. of cells: 69
Wing span: 13.33 m
Aspect ratio: 5.74
Min sink: 1 m/s
Max speed: 50 kph

Fancy 28
Paraglider circa 1998.
Wing area: 28 sq.m
Pilot weight: 65-85 kg
No. of cells: 44
Wing span: 11.15 m
Aspect ratio: 4.45
Min sink: 1.2 m/s
Max speed: 40 kph
Fancy 30
Paraglider circa 1998.
Wing area: 29.6 sq.m
Pilot weight: 80-100 kg
No. of cells: 40
Wing span: 11.68 m
Aspect ratio: 4.61
Min sink: 1.2 m/s
Max speed: 40 kph

With a chassis designed to work in extreme conditions and on professional jobs, there are 2 sizes: 1450 and 1400. Both have 200 cc power with Carbon Tripal propellers (recommended 130cm).
The engine can fly 4-5 hours and then carry out two seater flights.

The chassis can be dismantled into 4 stainless steel parts, or on request at 2, 3, or 5 parts. They are TIG welded, using stainless steel pipes, 304 & 316 grade in 6, 8, 10, 12 and 16 mm in the central part of the chassis frame. The 16 mm tube offers a double impact resistance.
There were more than 15 models of chassis, to mount any engine or incorporate the Evolution & Fly 100 EVO range of light engines,
Price 2009: US$1,650
F 200 1400
Engine: F 200, 200 cc
Carburettor: Walbro 37
Power: 27 hp
Belt reduction: 1 / 3
Cooling: Air
Clutch: No
Thrust: 78 kg
Fuel: 98 Green
Fuel tank: 14 lt
Consumption: 3 lt/hr
Frame dimensions: 130 x 130 x 27 cm
Prop: BA014 – Wood 125 or BA015 – 3 parts, Carbon 120 cm
Weight: 30 kg
Max pilot weight: 120 kg
Recomended pilot weight: 100 kg
Harness: Freedom
Parachute container: Down System
Parachutes sling: Serial
F 200 1450
Engine: F 200, 200 cc
Carburettor: Walbro 37
Power: 27 hp
Belt reduction: 1 / 3
Cooling: Air
Clutch: No
Thrust: 82 kg
Fuel: 98 Green
Fuel tank: 14 lt
Consumption: 3 lt/hr
Frame dimensions: 140 x 140 x 27 cm
Prop: BA016 – 3 parts, Carbon 130 cm
Weight: 31.5 kg
Max pilot weight: 200 kg+ Tandem
Recomended pilot weight: 125+ kg
Harness: Freedom
Parachute container: Down System
Parachutes sling: Serial

The first generation of the DHV 1-2 Atis glider was voted as the glider of a year by VOL LIBRE. The Atis 2 has new certification EN-B based on CEN 926-1 and 926-2, new profile, new layout and new experience.
(EN B equals the DHV 1-2 classification of the glider, the certification is different, and CEN 926-2 is different from DHV certification!)
The main changes compared to the first generation of the glider:
New profile with lighter ribs concept and higher speed range
New layout scheme
New design of stabilizers
Higher speed range with lower sink and higher glide efficiency
New, easy to use and highly efficient speed system
New geometry
New technology of the leading edge design
Trailing edge with velcro opening for easy cleaning of the canopy
Atis 2 (DHV 1-2) Price 2009: US$3,500.00
The Sky Paragliders Atis Acro model intended for Acro pilots is based in Sky’s intermediate glider, the Atis, released in 2002 in 3 sizes and about to have certification for the 4th, an XS (DHV 1-2). The Atis Acro had a good debut in the hands of pilot Tomas Lednik, who took the 3rd place at the past Oludeniz Air Games in Turkey with it. It is a small glider (XS size) and favoured with more speed and dynamic response than the serial model, thanks to a different plan layout.

ATIS 2SMLXL
Layout surface: 23,11 sq.m
Layout span: 10,86 m
Layout aspect ratio: 5,10
Projected surface: 20,69 sq.m
Projected span: 9,10 m
Projected aspect ratio: 4,00
Number of cells: 53
Weight of the glider: 5,0 kg
Take-off load: 60-80 kg
Trim speed: 37 km/h
Minimum speed: 23 km/h
Maximum speed: 48 km/h
Max. gliding ratio: 8,5
Min. sink rate: 1,15 m/s
Test: EN B
ATIS 2SMLXL
Layout surface: 25,00 sq.m
Layout span: 11,29 m
Layout aspect ratio: 5,10
Projected surface: 22,38 sq.m
Projected span: 9,47 m
Projected aspect ratio: 4,00
Number of cells: 53
Weight of the glider: 5,2 kg
Take-off load: 75-95 kg
Trim speed: 37 km/h
Minimum speed: 23 km/h
Maximum speed: 48 km/h
Max. gliding ratio: 8,5
Min. sink rate: 1,15 m/s
Test: EN B
ATIS 2SMLXL
Layout surface: 26,65 sq.m
Layout span: 11,66 m
Layout aspect ratio: 5,10
Projected surface: 23,86 sq.m
Projected span: 9,77 m
Projected aspect ratio: 4,00
Number of cells: 53
Weight of the glider: 5,4 kg
Take-off load: 87-110 kg
Trim speed: 37 km/h
Minimum speed: 23 km/h
Maximum speed: 48 km/h
Max. gliding ratio: 8,5
Min. sink rate: 1,15 m/s
Test: EN B
ATIS 2SMLXL
Layout surface: 28,83 sq.m
Layout span: 12,12 m
Layout aspect ratio: 5,10
Projected surface: 25,80 sq.m
Projected span: 10,16 m
Projected aspect ratio: 4,00
Number of cells: 53
Weight of the glider: 5,7 kg
Take-off load: 105-130 kg
Trim speed: 37 km/h
Minimum speed: 23 km/h
Maximum speed: 48 km/h
Max. gliding ratio: 8,5
Min. sink rate: 1,15 m/s
Test: EN B