Ultralight / ULM and LSA Aircraft for Sport Pilots
This is a collection of the aircraft at pilotmix.com that are either classified as LSA or ULM / Ultralights.
Some of these aircraft are also classified as homebuilts since they are sold as kits and you have to assemble them yourself.
So have you ever dreamed about owning your own airplane? Browse these aircraft and follow the links to read more about them.
[sort by aircraft model]
Stall: 34 kt | 39 mph | 63 kmh
Cruise: 94 kt | 109 mph | 175 kmh
VNE: 117 kt | 134 mph | 216 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 740 ft | 225 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: The 3Xtrim is a single-engine, two-seater monoplane with braced high wing, conventional controls and fixed three-wheel landing gear. The front-mounted engine is coupled to a two-blade or three-blade (depending on version) adjustable pulling propeller. A spacious, heated and ventilated cockpit with seats in one row and a large baggage compartment make the airplane comfortable, silent and well furbished. Access is easy through doors on each side opening upwards and supported in this position by gas springs.
Fixed three-wheel landing gear with castoring front wheel, composite main spring and hydraulic disc brakes, ensures safe take-off and landing on all types of airport surfaces, grass included.
The Ballistic Rescue System (BRS5) provides protection for the passengers and aircraft at altitudes above 30 m and speeds up to 235 kmph (145 mph). The aircraft structure is fabricated from composites based on epoxy resin with glass and carbon fibre. This totally composite structure reduces necessary maintenance work to pre-flight inspection and cleaning.
The aircraft fully complies with the JAR-VLA requirements and has a Type Certificate of Very Light Airplane. Excellent flight characteristics make this aircraft a perfect choice for primary schooling, training, travelling, and recreation. The aircraft is just as suitable for patrol flights and aerial photography. Flying is precise, easy, safe, and pleasant. Thanks to the incorporated technical solutions, components and materials, operational costs are low and comparable with a medium-class passenger car. A three-years manufacturer\'s warranty is standard.
The aircraft is manufactured in three versions:
* ULA - \"Ultra Light Aircraft\"
* AULA - \"Advanced Ultra Light Aircraft\"
* VLA - \"Very Light Aircraft\"
Text and photo from: www.3xtrim.pl
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Price: Not given
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Stall: 35 kt | 40 mph | 65 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 97 kt | 112 mph | 180 kmh
Empty Weight: 300 kg | 661 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 9
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 820 ft | 250 m
Aircraft information: Originally the Petrel amfibian.
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The Seastar, whose design now go back for over 10 years, originates from France and Brazil.
Seastar, a variation from the original concept, has a larger enclosed cockpit designed especially with the North American pilot size and requirement in mind. The hull is wider and slightly longer from the previous models and an improved step in the hull, enhances water take-off capability greatly. A longer lower wing with the fuel tank in the wings adds to flying safety and overall performance. These additional design changes have made the Seastar the most advanced and desirable amphibian airplane on the market today. There are nearly one hundred units Seastar type aircraft flying throughout the world today.
Currently the Seastar is only available as a kit, but soon, AAC Amphibian Airplanes of Canada LTD will be supplying the North American and Worldwide markets with the ready to fly Light Sportsplane version of the Seastar, to be known as the SeaLoon. The complete "Seastar fast build kit" consisting of all structural noble hardware and components will still be available for the foreseeable future.
Our goal is to have a good relationship with Seastar owners and builders, similar to that of the "Airstream Organization", and to build a product with utmost emphasis on safety and reliability. We will strive to promote future products, get-togethers and air ventures worldwide. We look forward to having each Seastar owner as a personal friend and potential representative of the Seastar fraternity with good long-lasting relationships with everyone worldwide.
Text from: http://www.seastaramphibian.com/
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Price: Not given
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Stall: 13 kt | 16 mph | 25 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 800 ft/min | 4-8 m/s
Glide Ratio: 1:3
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: ultrilight high performance autogyro kit or ready to fly
see http://www.absaerolight.com/
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Price: 65000 EURO
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Stall: 30 kt | 34 mph | 55 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 261 kg | 575 lbs
MTOW Weight: 431 kg | 950 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 250 ft | 76 m
Aircraft information: As early as the 1920s, Mr. Orland G. Corben believed that flying should not be a rich man's luxury. He saw the need for an aircraft that was properly designed, inexpensive to build, and safe and easy to fly. To recognize this goal, Mr. Corben created the first homebuilt airplane, the Baby Ace. In 1954, Paul Poberenzy, who a year earlier had founded the still fledgling Experimental Aircraft Association, built a Baby Ace aircraft as a three part series in Mechanix Illustrated. The success of the articles caused an explosion in the homebuilt movement. The Baby Ace that Mr. Poberenzy built for Mechanix Illustrated is now in the EAA AirVenture Museum.
Today, you can build and own an aircraft with a history almost as old as powered flight itself. The Ace Aircraft Company offers plans and kits for the single place Baby Ace Model D and the two place Junior Ace Model E aircraft, and we are currently pursuing FAA certification to build Ace aircraft ready to fly away. And all Ace aircraft meet the standards for the new Light-Sport Aircraft category. Indeed, Mr. Corben's dream in the 1920s of well designed, inexpensive, and safe homebuilt aircraft is still being realized today.
The price is for kit.
Text and Photo from http://www.aceaircraft.net/
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Price: 18950 USD
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Stall: 38 kt | 44 mph | 71 kmh
Cruise: 91 kt | 105 mph | 169 kmh
VNE: 113 kt | 130 mph | 209 kmh
Empty Weight: 293 kg | 645 lbs
MTOW Weight: 556 kg | 1225 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 600 ft | 183 m
Landing distance (50ft obstacle): 300 ft | 91 m
Aircraft information: As early as the 1920s, Mr. Orland G. Corben believed that flying should not be a rich man's luxury. He saw the need for an aircraft that was properly designed, inexpensive to build, and safe and easy to fly. To recognize this goal, Mr. Corben created the first homebuilt airplane, the Baby Ace. In 1954, Paul Poberenzy, who a year earlier had founded the still fledgling Experimental Aircraft Association, built a Baby Ace aircraft as a three part series in Mechanix Illustrated. The success of the articles caused an explosion in the homebuilt movement. The Baby Ace that Mr. Poberenzy built for Mechanix Illustrated is now in the EAA AirVenture Museum.
Today, you can build and own an aircraft with a history almost as old as powered flight itself. The Ace Aircraft Company offers plans and kits for the single place Baby Ace Model D and the two place Junior Ace Model E aircraft, and we are currently pursuing FAA certification to build Ace aircraft ready to fly away. And all Ace aircraft meet the standards for the new Light-Sport Aircraft category. Indeed, Mr. Corben's dream in the 1920s of well designed, inexpensive, and safe homebuilt aircraft is still being realized today.
The price is for kit.
Text and Photo from http://www.aceaircraft.net/
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Price: 20950 USD
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Stall: 31 kt | 36 mph | 58 kmh
Cruise: 65 kt | 75 mph | 121 kmh
VNE: 83 kt | 95 mph | 153 kmh
Empty Weight: 295 kg | 650 lbs
MTOW Weight: 559 kg | 1232 lbs
Climb Ratio: 1100 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 150 ft | 46 m
Landing distance (50ft obstacle): 150 ft | 46 m
Aircraft information: The Aventura II is a 2 seat, experimental category amphibious aircraft, that the average person can build (really!) in about 225 hours for the basic model. Different options and some engines will add to the build time. General specifications and options for the model are shown below, with links to performance information for specific engines.
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Editors note: Take-off and landing distance on land and not over 50ft obstacle
Text and Photo from: http://www.aeroadventureinc.com
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Price: Not given
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Stall: 30 kt | 35 mph | 56 kmh
Cruise: 91 kt | 104 mph | 168 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 500 kg | 1102 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: -
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Price: Not given
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Stall: 30 kt | 34 mph | 55 kmh
Cruise: 92 kt | 106 mph | 170 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 260 kg | 573 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 900 ft/min | 4.5 m/s
Glide Ratio: 1:12
Take-off distance (50ft obstacle): 820 ft | 250 m
Landing distance (50ft obstacle): 490 ft | 150 m
Aircraft information: -
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Price: Not given
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Stall: 32 kt | 37 mph | 60 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 92 kt | 106 mph | 170 kmh
Empty Weight: 230 kg | 507 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 600 ft/min | 3,5 m/s
Glide Ratio: 1:12
Take-off distance (50ft obstacle): 980 ft | 300 m
Landing distance (50ft obstacle): 660 ft | 200 m
Aircraft information: info and photo from: www.aeroservices.fr
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Price: Not given
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Stall: 39 kt | 45 mph | 72 kmh
Cruise: 103 kt | 119 mph | 191 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 210 kg | 463 lbs
MTOW Weight: 480 kg | 1058 lbs
Climb Ratio: 900 ft/min | 4.32 m/s
Glide Ratio: 15
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: -
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Price: Not given
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Stall: 30 kt | 35 mph | 56 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 261 kg | 575 lbs
MTOW Weight: 590 kg | 1300 lbs
Climb Ratio: 1500 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 400 ft | 122 m
Landing distance (50ft obstacle): 400 ft | 122 m
Aircraft information: Merlin
All data is for wheel version.
The price is for complete Wing Kit, Fuselage Kit, Covering Kit, Rotax 912 Powerplant, Rotax 912 Installation Kit.
Photo from: www.aerocompinc.com
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Price: 35995 USD
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Stall: 32 kt | 37 mph | 60 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 250 kg | 551 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 13
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 300 ft | 90 m
Aircraft information: Available in kit or as ready built.
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Price: Not given
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Stall: 22 kt | 25 mph | 40 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 20 ft | 5 m
Aircraft information: High performance autogyro
http://www.aerocopter-europa.com/
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Price: Not given
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Stall: 31 kt | 35 mph | 57 kmh
Cruise: 105 kt | 121 mph | 195 kmh
VNE: 130 kt | 149 mph | 240 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 495 kg | 1091 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 13:1
Take-off distance (50ft obstacle): 200 ft | 60 m
Landing distance (50ft obstacle): 390 ft | 120 m
Aircraft information: Text & Photo from http://aerodynosdecolombia.com
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Price: Not given
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Stall: 30 kt | 34 mph | 55 kmh
Cruise: 124 kt | 143 mph | 230 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Isatis 01
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Price: Not given
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Stall: 0 kt | 0 mph | 0 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 385 kg | 849 lbs
MTOW Weight: 650 kg | 1433 lbs
Climb Ratio: 2000 ft/min | 10 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Aerokopter Group - light helicopters manufacturer. www.aerokopter.com
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Price: 150000 USD
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Stall: 27 kt | 31 mph | 50 kmh
Cruise: 89 kt | 103 mph | 165 kmh
VNE: 124 kt | 143 mph | 230 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1600 ft/min | 8 m/s
Glide Ratio: 1:5
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 660 ft | 200 m
Aircraft information: The fruit of innovation and the will of the company to continue improving, we have developed the new Stela model at a very competitive price.
This new ultralight maintains all the characteristics and reliability of its predecessor Moragón M-1, but with improved performance.
Text and photo from: http://www.aeromoragon.net/enuestroavion.htm
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Price: 42000 EURO
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Stall: 31 kt | 36 mph | 58 kmh
Cruise: 127 kt | 146 mph | 235 kmh
VNE: 157 kt | 180 mph | 290 kmh
Empty Weight: 295 kg | 650 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 2000 ft/min | 10 m/s
Glide Ratio: 15:1
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Text and photo from: http://www.aeronix.fr/
Three-axis ULM, two-seater side by side, with median wing, twin-engine
push-pull, canard formula, tricycle landing gear, composites construction
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Price: Not given
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Stall: 32 kt | 37 mph | 60 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 113 kt | 130 mph | 210 kmh
Empty Weight: 230 kg | 507 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 10
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 490 ft | 150 m
Aircraft information: The DAR-21 airplane, is a two-seat vehicle, used a wide range of engines from two stroke ROTAX engine – 582 series, 65 HP to 4 cylinder 4 stroke Jabiru 2200 - 80 HP.
Aluminium alloys 1050, 2024, 3105 and 6061 are the basic buiding materials of the DAR-21 airplane.
DAR – 21 S is based on 2024 and 6061 aluminum alloys.
DAR21 Tropic is based on using the soft 1050 and 3105 aluminum alloys. These materials are softer, but with better anticorrosion quality.
The welded metal parts are made of lowcarbonic structure steel 4130, while turnery and milling parts are made of structure steel 4340.
The cabin is fully closed, with tandem seats /one behind the other/. There is only one door on the right side giving access both to seats and cargo sector. All necessary navigation and engine control instruments are set in one panel. The operating of airplane is double and lets you control the vehicle both from front and rear seats.
Text from: http://www.dar.dir.bg/dar21-en%20tech.htm
Pricing:
EXW SOF (Ex-work Sofia, Bulgaria) prices:
Complete airplanes:
DAR-21 with ROTAX 912 – 31500 EUR
DAR-21 with Jabiru 2200 – 31450 EUR
Kit Pricing EWR SOF:
DAR-21 kit without engine, prop and instruments – 20700 EUR
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Price: Not given
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Stall: 24 kt | 28 mph | 45 kmh
Cruise: 49 kt | 56 mph | 90 kmh
VNE: 65 kt | 75 mph | 120 kmh
Empty Weight: 195 kg | 430 lbs
MTOW Weight: 380 kg | 838 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 6
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 330 ft | 100 m
Aircraft information: All metal construction
Pricing:
EXW SOF (Ex-work Sofia, Bulgaria) prices:
Complete airplanes:
DAR-23 with HKS 700 E – 17500 EUR
Kit Pricing EWR SOF:
DAR-23 kit without engine, prop and instruments – 10500 EUR
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Price: Not given
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Stall: 35 kt | 40 mph | 65 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 280 kg | 617 lbs
MTOW Weight: 500 kg | 1102 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 10
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 490 ft | 150 m
Aircraft information: Little bit bigger than DAR-21
Pricing:
Direct Sales Price in France, by "Aeroplanes DAR France" Sarl
Complete airplanes
DAR-21 S with ROTAX 582 – 30840 EUR HT & 36885 EUR TTC
DAR-21 S with ROTAX 912 – 38225 EUR HT & 45717 EUR TTC
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Price: Not given
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Stall: 32 kt | 37 mph | 60 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 127 kt | 146 mph | 235 kmh
Empty Weight: 113 kg | 250 lbs
MTOW Weight: 204 kg | 450 lbs
Climb Ratio: 1800 ft/min | 9 m/s
Glide Ratio: 10
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 490 ft | 150 m
Aircraft information: DAR Speedster The design team of Aeroplanes DAR, has the ambitious goal to modify the existing models DAR-21 First serious change is the new wing. The new wing increases the airplane performance. The result indicated 17-20 percent better wing performance than the original design. Second serious change is made in the fuselage. The structure of airframe is new with reduced weight, while increasing the rigidity. Again, as with the wings, the new advanced technology help to achieve better results and to keep the general outside lines of the machine, because this design was very well accepted by the customers. The DAR Speedster continues this design line, with ‘small” elegant changes. Many details have been redesigned and improved, giving a more ennoble view of the fuselage and airplane. All of these "small" changes have also aerodynamic reason and we have eliminated most of the parts that produced addition
al drag.
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Price: 30000 EURO
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Stall: 23 kt | 26 mph | 42 kmh
Cruise: 49 kt | 56 mph | 90 kmh
VNE: 65 kt | 75 mph | 120 kmh
Empty Weight: 110 kg | 243 lbs
MTOW Weight: 220 kg | 485 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: 10
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 330 ft | 100 m
Aircraft information: Single seater under FAR103 rule.
Composite (Carbon Fiber) pod and metal wings.
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Price: 6800 EURO
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Stall: 26 kt | 30 mph | 48 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 106 kt | 122 mph | 196 kmh
Empty Weight: 258 kg | 569 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1100 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 490 ft | 150 m
Aircraft information: Although a modern aircraft in concept the Aeroprakt A22 Foxbat uses a very conventional method of construction in riveted aluminium. Each kit is supplied with the fuselage, wings, tailplane, fin and all control surfaces pre-riveted.
The pictures show the airframe kit exactly as it comes out of the crate. The remaining riveting work is confined to final fitting of the floor-pan (which is already "cleco'd" in place) and securing the fin and various mounting brackets and webs to the bare fuselage monocoque. Three special holding cradles are required during this stage of the construction and we provide these on free loan. The rest of the work consists of fitting the engine and ancillaries, the control mechanisms (torque tubes, push rods, bell-cranks, etc) all of which are factory finished, anodised and ready to install. No fabrication of components is required (each component bearing surface even has a pressed in aerospace-quality rose-joint).
After installing the under-carriage and wheels the final finishing involves covering and painting, and fitting the instrument panel, etc. A A-22 Foxbat kit can be assembled in 500 hours by one person, or less with an assistant. One person can complete most of the assembly but some jobs will need an extra pair of hands. With good planning a largish domestic garage will be a big enough workshop space to complete all the sub-assemblies including covering and painting. Obviously a larger space is required for the complete assembly of the aircraft although that could be done outdoors prior to final Inspection and transport to the airfield for test flying. A folding wing option is available.
Text and photo from: http://www.foxbat.co.uk/spec.htm
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Price: Not given
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Stall: 35 kt | 40 mph | 64 kmh
Cruise: 103 kt | 118 mph | 190 kmh
VNE: 111 kt | 128 mph | 206 kmh
Empty Weight: 288 kg | 636 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 14:1
Take-off distance (50ft obstacle): 400 ft | 122 m
Landing distance (50ft obstacle): 460 ft | 140 m
Aircraft information: www.RLSA.us
www.eurofox-usa.com
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Price: 39500 EURO
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Stall: 40 kt | 46 mph | 74 kmh
Cruise: 100 kt | 115 mph | 185 kmh
VNE: 130 kt | 150 mph | 241 kmh
Empty Weight: 220 kg | 485 lbs
MTOW Weight: 750 kg | 1653 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 260 ft | 79 m
Landing distance (50ft obstacle): 300 ft | 91 m
Aircraft information: www.aeropup.com
Fast folding wings enable one person to swing the wings back to trailer width without help in minutes, Australian made and looking for overseas distributors.
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Price: 18000 USD
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Stall: 35 kt | 40 mph | 65 kmh
Cruise: 103 kt | 118 mph | 190 kmh
VNE: 130 kt | 149 mph | 240 kmh
Empty Weight: 285 kg | 628 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 580 ft | 178 m
Landing distance (50ft obstacle): 630 ft | 192 m
Aircraft information: A single-engine all-composite high-wing side-by-side two-seater with a fixed tricycle landing gear (a steerable nose wheel included). The aircraft design and construction is determined to recreational flying as well as flight training. Provided by a sufficient level of an aircraft equipment then any realization of long distance cross-country flights is also possible. Those aspects are emphasized by easy manoeuvrability of this aircraft and by a comfortable space solution of its cockpit with a roomy baggage compartment behind fully adjustable seats.
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Price: 48500 EURO
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Stall: 34 kt | 39 mph | 63 kmh
Cruise: 130 kt | 150 mph | 241 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Photo by Daniel Mattsson.
The Dynamic WT-9 is the work of Wala Tadeas. As its designation WT 9 indicates it, is his ninth project. Aerospool's long-term production and fabrication of gliders and glider components over the years has given them the ability to produce strong lightweight aircraft with great flight qualities. (Aerospool is one of the main subcontractors for Schempp-Hirth glider company.)
http://www.lightsportaviation.se
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Price: 60000 EURO
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Stall: 36 kt | 41 mph | 66 kmh
Cruise: 101 kt | 116 mph | 187 kmh
VNE: 130 kt | 150 mph | 241 kmh
Empty Weight: 388 kg | 855 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 770 ft/min | 4 m/s
Glide Ratio: 1:12
Take-off distance (50ft obstacle): 1246 ft | 380 m
Landing distance (50ft obstacle): 951 ft | 290 m
Aircraft information: Text and photo from: www.lightsportflying.com
The Festival, manufactured by SC Aerostar S.A. of Romania, (of YAK-52 fame) is a ready-to-fly, FAA certified, Special Light Sport Aircraft, and has been designed with one idea in mind: To create an affordable airplane which is safe, simple, and easy to inspect, maintain and operate.
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Price: Not given
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Stall: 35 kt | 40 mph | 64 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 132 kt | 152 mph | 245 kmh
Empty Weight: 295 kg | 650 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5.1 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: With the engine choice contrary to many other manufacturers another path was taken:
We selected a modified BMW fuel injection engine, which has its origin in the building of motorcycles. This engine of in the UL scene admitted Trike manufacturer "Take off" reequipped. The special characteristics of this engine generation are:
- standard fuel injection system
- catalyst optionally possible
- smaller consumption
- better launch characteristics
- favorable mass production technology
- no carburetor icing
The engine in aerostyle Breezer can convince also by its calm, strong run, as well as its pleasant clay/tone
With a view under the Cowling immediately the clear and low-maintenance installation of the engine as well as the associated aggregates is noticeable.
Since however many ultralight aircraft prefer the Rotax 912, in 2001 a Aerostyle Breezer was equipped with a Rotax 912 S and certified. Other engine concepts are at present in the development, and/or in planning - let surprise itself!
Text and photo from: http://www.aerostyle-gmbh.de/
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Price: Not given
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Stall: 38 kt | 43 mph | 70 kmh
Cruise: 140 kt | 162 mph | 260 kmh
VNE: 173 kt | 199 mph | 320 kmh
Empty Weight: 370 kg | 816 lbs
MTOW Weight: 650 kg | 1433 lbs
Climb Ratio: 1800 ft/min | 9 m/s
Glide Ratio: 15
Take-off distance (50ft obstacle): 720 ft | 220 m
Landing distance (50ft obstacle): 590 ft | 180 m
Aircraft information: Modern two seat composite aircraft, that is comfortable, has excellent panoramic visibility, and perfectly aerodynamic to the a high cruise speed. Designers: Daniel & Marek Debski
Structure: Composite construction reinforced by glass and carbon fibres.
Power Plant: Aircraft Compact Piston Engine (2 x 100hp, two engines in one ), for the high performance and for the high safety level.
We look for serious partners for co-peration
More info: http://dkd1970.webpark.pl/ , http://nasc.meil.pw.edu.pl/ACE.HTM
Contact: dedal@ilot.edu.pl
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Price: Not given
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Stall: 43 kt | 50 mph | 80 kmh
Cruise: 92 kt | 106 mph | 170 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 450 kg | 992 lbs
MTOW Weight: 700 kg | 1543 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 9
Take-off distance (50ft obstacle): 300 ft | 90 m
Landing distance (50ft obstacle): 390 ft | 120 m
Aircraft information: DEKO-8 VLA Club is under design now, by Polish aeronautical engineers: Daniel Debski Ph.D., Marek Debski Ph.D. and Krzysztof Kotlinski. M.Sc. Structure: Aluminum tube fuselage with composite joints (Polish Patent) and with Ceconite covering. Power Plant: PZL Franklin F4 (135 hp) with a three-blade MT- Propeller, variable-pitch propeller.
We are looking for Project Partners.
Information and Contact: http://www.dkd1970.webpark.pl/
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Price: Not given
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Stall: 40 kt | 47 mph | 75 kmh
Cruise: 146 kt | 168 mph | 270 kmh
VNE: 216 kt | 249 mph | 400 kmh
Empty Weight: 420 kg | 926 lbs
MTOW Weight: 700 kg | 1543 lbs
Climb Ratio: 2000 ft/min | 10 m/s
Glide Ratio: 16
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 660 ft | 200 m
Aircraft information: Two seat modern composite aircraft with super panoramic visibility (only comparable with that of a helicopter), low cockpit noise levels and perfectly aerodynamic to the high cruise speed. Designer: Daniel K. Debski D.Sc. (Warsaw University of Technology)
Structure: Composite construction reinforced by glass and carbon fibres.
Power Plant: Aircraft Compact Piston Engine (2 x 100hp, two engines in one), for the high performance and for the high safety level. Option:125 -200hp one Piston Engine.
We look for serious partners for co-operation
More info and contact: http://dkd1970.webpark.pl/ http://nasc.meil.pw.edu.pl/ACE.HTM
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Price: Not given
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Stall: 38 kt | 43 mph | 70 kmh
Cruise: 120 kt | 138 mph | 222 kmh
VNE: 162 kt | 186 mph | 300 kmh
Empty Weight: 380 kg | 838 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 1800 ft/min | 9 m/s
Glide Ratio: 14
Take-off distance (50ft obstacle): 390 ft | 120 m
Landing distance (50ft obstacle): 460 ft | 140 m
Aircraft information: DEKO-15 LSA is design conception of Light Sport Aircraft. This is two place, side-by-side, composite-metal aircraft, with excellent panoramic visibility and perfectly aerodynamic to the high cruise speed. The new fast cruiser without compromise! Designers: Daniel Debski Ph.D. (Warsaw University of Technology) & Marek Debski Ph.D. (Institute of Aviation)
Structure: Composite construction reinforced by glass and carbon fibers, and with composite joints.
Power Plant: Aircraft Compact Piston Engine (2 x 80hp, two engines in one - new idea), for the high performance and for the high safety level. Option 1x 160 hp)
We look for serious partners for co-peration
More info: http://dkd1970.webpark.pl/ , http://nasc.meil.pw.edu.pl/research.htm http://nasc.meil.pw.edu.pl/ACE.HTM
Contact: daniel.debski@ipbm.simr.pw.edu.pl dedal@ilot.edu.pl
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Price: Not given
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Stall: 23 kt | 26 mph | 42 kmh
Cruise: 52 kt | 60 mph | 97 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 175 kg | 386 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Text and photo from: http://www.aerotrike.co.za
The specs varies depending on the wing used. There is many options.
The Aerotrike is one of the world's most advanced ultralight/ microlight trikes. This type of aircraft is becoming increasingly popular the world over as an incredibly safe and enjoyable means of recreational flight. The comparatively low purchase and maintenance costs also make it the ideal choice for someone wishing to fly!
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Price: Not given
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Stall: 23 kt | 26 mph | 42 kmh
Cruise: 48 kt | 55 mph | 89 kmh
VNE: 65 kt | 75 mph | 121 kmh
Empty Weight: 114 kg | 252 lbs
MTOW Weight: 272 kg | 600 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 1:9
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 300 ft | 91 m
Aircraft information: Text and photo from: www.aerolite103.com
Also available as kit.
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Price: Not given
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Stall: 23 kt | 27 mph | 43 kmh
Cruise: 56 kt | 65 mph | 105 kmh
VNE: 74 kt | 85 mph | 137 kmh
Empty Weight: 115 kg | 254 lbs
MTOW Weight: 245 kg | 540 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: The Affordaplane was introduced in 2001 as a simple to build, affordable ultralight. Featuring three axes, full span ailerons, and classic lines, the Affordaplane has gathered a lot of attention since its release.
Photo and text from: www.affordaplane.com
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Price: 3000 USD
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Stall: 35 kt | 40 mph | 65 kmh
Cruise: 65 kt | 75 mph | 120 kmh
VNE: 86 kt | 99 mph | 160 kmh
Empty Weight: 252 kg | 556 lbs
MTOW Weight: 475 kg | 1047 lbs
Climb Ratio: 800 ft/min | 4.0 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 590 ft | 180 m
Aircraft information: - The UCL MAJA year:2004 is a two place single-engine, high wing airplane of conventional configuration consisting of a composite fuselage and wood wings. It is equipped with a fixed tricycle landing gear.
Very good condition!!!
+4g/-2g
more info:
dejan_pelivanoski@hotmail.com
Dejan Pelivanoski
9TH Septemvri No:46
7500 Prilep
Macedonia
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Price: 20 EURO
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Stall: 28 kt | 32 mph | 51 kmh
Cruise: 63 kt | 72 mph | 116 kmh
VNE: 100 kt | 115 mph | 185 kmh
Empty Weight: 191 kg | 420 lbs
MTOW Weight: 476 kg | 1050 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 300 ft | 91 m
Aircraft information: KITS COME IN COMPLETE FORMAT WITH ALL ACCESSORIES 3 BLD GA PROP, PAINT, BRAKES, ENGINE ACCESSORIES, TUNDRA TIRES, INSTRUMENTS, AVAILABLE WITH FLOATS, AMPHIB GEAR AND SKIS
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Price: 17995 USD
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Stall: 28 kt | 32 mph | 51 kmh
Cruise: 72 kt | 83 mph | 134 kmh
VNE: 100 kt | 115 mph | 185 kmh
Empty Weight: 209 kg | 460 lbs
MTOW Weight: 476 kg | 1050 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 300 ft | 91 m
Aircraft information: Chinook PLUS 2 With 582
Comes complete with all parts and accessories, 3 bld g.a. prop, paint package, instruments, brakes, tundra tires, engine accessories. Full Lotus floats and amphib gear an option, Skis as well
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Price: 19995 USD
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Stall: 28 kt | 32 mph | 51 kmh
Cruise: 65 kt | 75 mph | 121 kmh
VNE: 100 kt | 115 mph | 185 kmh
Empty Weight: 218 kg | 480 lbs
MTOW Weight: 476 kg | 1050 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 300 ft | 91 m
Aircraft information: Complete kit with HKS engine, engine accessories, upright engine mount, superior ceconite fabric, paint, instruments, 3 BLD GA prop, tundra tires, brakes, dual throttle assembly, Options include Full Lotus Floats, Amphib gear, Skis - 200 hour build time
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Price: 20995 USD
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Stall: 30 kt | 35 mph | 56 kmh
Cruise: 72 kt | 83 mph | 134 kmh
VNE: 100 kt | 115 mph | 185 kmh
Empty Weight: 236 kg | 520 lbs
MTOW Weight: 476 kg | 1050 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 100 ft | 30 m
Landing distance (50ft obstacle): 350 ft | 107 m
Aircraft information: Cadillac of our Fleet, complete kit includes all part and accessories including 3 bld ground adj prop, paint package, upright engine mount, superior ceconite fabric, enclosed cabin, instruments, tundra tires, brakes, dual throttle assembly, complimentary tow bar-Makes an awesome float plane, Amphib gear available, skis, in-wing fuel tanks etc
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Price: 27500 USD
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Stall: 0 kt | 0 mph | 0 kmh
Cruise: 28 kt | 32 mph | 51 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 141 kg | 310 lbs
MTOW Weight: 431 kg | 950 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 5:1
Take-off distance (50ft obstacle): 100 ft | 30 m
Landing distance (50ft obstacle): 75 ft | 23 m
Aircraft information: Summit II Powered Parachute
Other engine options - Rotax 503, Rotax 912 and HKS engine. Anodized, 4 point pick up, true two place seating, ground steering, standard kit comes with airframe, engine, engine accessories, Digital EIS instrument readings, 3 bld GA prop, 500 Canopy. Lots of exciting, exclusive features
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Price: 15950 USD
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Stall: 26 kt | 30 mph | 48 kmh
Cruise: 58 kt | 67 mph | 108 kmh
VNE: 78 kt | 90 mph | 145 kmh
Empty Weight: 154 kg | 340 lbs
MTOW Weight: 295 kg | 650 lbs
Climb Ratio: 850 ft/min | 4 m/s
Glide Ratio: 7:1
Take-off distance (50ft obstacle): 90 ft | 27 m
Landing distance (50ft obstacle): 75 ft | 23 m
Aircraft information: Beaver SS
Complete kit includes airframe, engine, engine accessories, 3 Bld GA prop, paint package, front brake, standard wheels, upright engine mount, instruments steerable nosewheel, ceconite fabric, adapts to floats and skis -flies like a charm!!!!
Contact us at paulette@junction.net or see our website at www.ultralight.ca
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Price: 13150 USD
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Stall: 48 kt | 55 mph | 89 kmh
Cruise: 130 kt | 150 mph | 241 kmh
VNE: 161 kt | 185 mph | 298 kmh
Empty Weight: 318 kg | 700 lbs
MTOW Weight: 590 kg | 1300 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 800 ft | 244 m
Landing distance (50ft obstacle): 900 ft | 274 m
Aircraft information: Kit only. Plans available from Aircraft Spruce & Specialty Co.
Plan Price $180.00
The Wittman Tailwind is an historic aircraft design. It first flew in 1953, a few weeks before the birth of the Experimental Aircraft Association. It demonstrated exceptional flight efficiency, incorporating a number of aerodynamic design features which Steve Wittman had gleaned from his extensive air racing experience. Prospective homebuilders at that time were both incredulous and inspired by the Tailwind. It was the stuff of which dreams were made and can be credited with helping the fledgling EAA to grow. Jack Cox's excellent history of the Tailwind was published in the September 1993 issue of Sport Aviation.1
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Price: Not given
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Stall: 30 kt | 34 mph | 55 kmh
Cruise: 56 kt | 64 mph | 103 kmh
VNE: 68 kt | 78 mph | 126 kmh
Empty Weight: 155 kg | 341 lbs
MTOW Weight: 264 kg | 583 lbs
Climb Ratio: 950 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Our aircraft cover a wide range of historical aviation. From the most recognized aircraft flown in World War One, the scarlet red FOKKER DR-1 TRIPLANE flown by The Red Baron, Manfred Von Richthofen, to the most technologically advanced aircraft to come from the great war effort, The FOKKER D-VIII parasol (AKA The Flying Razor). Also available is the FOKKER E-III, Eindecker, the first plane to mount a synchronized machine gun and the FOKKER D-VI, the precursor of the FOKKER D-VII, probably the best performing aircraft used in the war by the German War Machine. New in 2001 is the Full Scale Nieuport 24. Also available from Airdrome Aeroplanes is the FULLY, FAA PART 103, LEGAL Dream Classic Ultralight.
Photo and text from http://www.airdromeaeroplanes.com/
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Price: Not given
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Stall: 23 kt | 26 mph | 42 kmh
Cruise: 47 kt | 54 mph | 87 kmh
VNE: 55 kt | 63 mph | 101 kmh
Empty Weight: 108 kg | 238 lbs
MTOW Weight: 212 kg | 468 lbs
Climb Ratio: 1150 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Quickbuild kit, 300 hours.
Photo and text from: http://www.airdromeaeroplanes.com/E-IIIA.htm
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Price: Not given
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Stall: 23 kt | 26 mph | 42 kmh
Cruise: 50 kt | 57 mph | 92 kmh
VNE: 55 kt | 63 mph | 101 kmh
Empty Weight: 109 kg | 241 lbs
MTOW Weight: 223 kg | 491 lbs
Climb Ratio: 850 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 200 ft | 61 m
Aircraft information: The dream classic is airdrome airplanes answer to the cry for an FAA legal, safe, three axis control system, back to basics ultralight aircraft.
The dream classic ultralight is a full three axis
aircraft with a side mount stick & is covered with
the certified poly fiber process. This kit comes
with all machining & required welding pre-done.
Construction time is normally around 100/120 man hours .
Text and photo from: http://www.airdromeaeroplanes.com/dream-classic.htm
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Price: Not given
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Stall: 35 kt | 40 mph | 64 kmh
Cruise: 76 kt | 87 mph | 140 kmh
VNE: 113 kt | 130 mph | 210 kmh
Empty Weight: 253 kg | 558 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: -
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Price: Not given
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Stall: 30 kt | 34 mph | 55 kmh
Cruise: 49 kt | 56 mph | 90 kmh
VNE: 97 kt | 112 mph | 180 kmh
Empty Weight: 278 kg | 613 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 400 ft/min | 2 m/s
Glide Ratio: 1:36
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Ultralight Motor Glider with retractable prop.
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Price: Not given
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Stall: 30 kt | 34 mph | 55 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 105 kt | 121 mph | 195 kmh
Empty Weight: 282 kg | 622 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1600 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 460 ft | 140 m
Landing distance (50ft obstacle): 510 ft | 155 m
Aircraft information: Text and Photo from: http://www.alisport.com/eu/eng/yuma.htm
Single engine, two-seater side-by-side
high-wing monoplane with a metal structure and
folding wings;
three versions with 4-stroke engines are available.
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Price: Not given
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Stall: 33 kt | 38 mph | 61 kmh
Cruise: 70 kt | 81 mph | 130 kmh
VNE: 97 kt | 112 mph | 180 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 510 kg | 1124 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: 26:1
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 820 ft | 250 m
Aircraft information: Text and Photo from: http://www.alpaero.com/
two-place side-by-side touring motorglider with front-mounted engine. Marketed as a basic kit available for homebuilders.
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Price: Not given
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Stall: 32 kt | 37 mph | 60 kmh
Cruise: 135 kt | 155 mph | 250 kmh
VNE: 154 kt | 177 mph | 285 kmh
Empty Weight: 285 kg | 628 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1400 ft/min | 7,5 m/s
Glide Ratio: 1:14
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 490 ft | 150 m
Aircraft information: Award Winner 2003 and 2004 in long distance race over 1200km with average speed of 254 km/h. Maximum Weight 450 -560 kg( depends on the certification-rules in different countries) The Pioneer 300 is a perfect combination of wonderful design, great performance, easy handling and immense safety. Available ready-to-fly and also in 2 different Kit-stages (51% and 80% ready)beginning at € 34500,- For more information contact Mr. Michael Reiss via phone:+49 1717854400
email:pioneer300@gmx.net
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Price: 66000 EURO
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Stall: 33 kt | 39 mph | 62 kmh
Cruise: 100 kt | 115 mph | 185 kmh
VNE: 130 kt | 149 mph | 240 kmh
Empty Weight: 260 kg | 573 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 1:11
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 390 ft | 120 m
Aircraft information: The Pioneer 200 is the perfect plane for flight-schools and aeroclubs as well as for the private pilot looking for an uncomplicated, reliable, easy to handle, goodlooking aircraft with good performance data.All this and much is available at an incredible price of € 21900,- for the 51% Kit and only €42500,- for a ready-to-fly aircraft.Need more information? Contact Mr. Michael Reiss via phone:+49 171 7854400 or email: pioneer300@gmx.net
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Price: 42500 EURO
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Stall: 32 kt | 37 mph | 60 kmh
Cruise: 135 kt | 155 mph | 250 kmh
VNE: 154 kt | 177 mph | 285 kmh
Empty Weight: 285 kg | 628 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: 1/14
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 490 ft | 150 m
Aircraft information: FULL OPTIONAL
450 Hr
For informatin
francoborin@libero.it
00393480166030
Venezia - Italy
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Price: 52000 USD
|
Stall: 23 kt | 27 mph | 43 kmh
Cruise: 48 kt | 55 mph | 89 kmh
VNE: 55 kt | 63 mph | 101 kmh
Empty Weight: 104 kg | 230 lbs
MTOW Weight: 209 kg | 460 lbs
Climb Ratio: 500 ft/min | 3 m/s
Glide Ratio: N/A
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 250 ft | 76 m
Aircraft information: July 2003 : The Eureka has been withdrawn from the market due to lack of resources. We will continue to answer all e-mail ! wstark@nucleus.com
The website will remain for informational purposes only.
http://www.nucleus.com/~eureka/
The Eureka was developed after recognizing that the current market does not offer an affordable Ultralight that is also easy to build.
Eureka is a machine that can be put into the air, ready-to-fly, for about $8000
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Price: 8000 USD
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Stall: 30 kt | 34 mph | 55 kmh
Cruise: 83 kt | 95 mph | 153 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 386 kg | 850 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 500 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 350 ft | 107 m
Landing distance (50ft obstacle): 350 ft | 107 m
Aircraft information: Text and photo from www.legend.aero
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Price: Not given
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Stall: 24 kt | 28 mph | 45 kmh
Cruise: 52 kt | 60 mph | 97 kmh
VNE: 66 kt | 76 mph | 122 kmh
Empty Weight: 115 kg | 254 lbs
MTOW Weight: 249 kg | 550 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 16:1
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Other Mitchell Wing websites: http://www.mitchellwing.com
News group:
http://groups.yahoo.com/group/mitchellwing/
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Price: 11700 USD
|
Stall: 33 kt | 38 mph | 61 kmh
Cruise: 127 kt | 146 mph | 235 kmh
VNE: 157 kt | 180 mph | 290 kmh
Empty Weight: 235 kg | 518 lbs
MTOW Weight: 470 kg | 1036 lbs
Climb Ratio: 1259 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 620 ft | 190 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Light Two-seater Motorgliders Family
- for all reasons and seasons
- soaring, towing, cruising,training
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Price: Not given
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Stall: 35 kt | 40 mph | 64 kmh
Cruise: 138 kt | 159 mph | 256 kmh
VNE: 165 kt | 190 mph | 305 kmh
Empty Weight: 250 kg | 551 lbs
MTOW Weight: 470 kg | 1036 lbs
Climb Ratio: 1437 ft/min | 7 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Light Two-seater Motorgliders Family
- for all reasons and seasons
- soaring, towing, cruising,training
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Price: Not given
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Stall: 43 kt | 50 mph | 80 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 325 kg | 717 lbs
MTOW Weight: 470 kg | 1036 lbs
Climb Ratio: 700 ft/min | 3.5 m/s
Glide Ratio: 35
Take-off distance (50ft obstacle): 1400 ft | 428 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Retractable landing gear, folding propeller, Reliable low-noise four-stroke engine, good gliding performance, suitable for trailering, one-man assembly possible, comfortable cockpit.
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Price: Not given
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Stall: 52 kt | 60 mph | 96 kmh
Cruise: 113 kt | 130 mph | 210 kmh
VNE: 130 kt | 149 mph | 240 kmh
Empty Weight: 330 kg | 728 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 890 ft | 270 m
Landing distance (50ft obstacle): 1530 ft | 465 m
Aircraft information: Homebuilt version of the 1944 BA-4. The BA-4B first flew in 1966.
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Price: Not given
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Stall: 35 kt | 40 mph | 64 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 97 kt | 112 mph | 180 kmh
Empty Weight: 274 kg | 604 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 460 ft | 140 m
Landing distance (50ft obstacle): 660 ft | 200 m
Aircraft information: Photo from: www.ul-bolaget.se
Text from: http://www.halley.hu/
The Apollo Fox is built according to the "BCAR” Section S constuction norm.
The aircraft has welded steel alloy tube fuselage covered with „ceconite” fabric. The wing are made of aluminium alloy both spars and ribs and then covered with ceconite. Wing can be folded backwards. One pilote can do it within 10 minits. The landing gears are aluminium plate sheet as year suspension. Wheels are equipped with hidraulic disc or mechanical drum brakes. Apollo Fox has very good rudder harmony and very easy to fly and land.
Available tail or nose wheel configurations.
Engine: Rotax 582 UL Mod 99 (65Hp), 912UL (80 Hp), 912 ULS (100 Hp), Jabiru 2200 (80Hp), Subaru EA 81 (100 Hp).
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Price: Not given
|
Stall: 39 kt | 45 mph | 72 kmh
Cruise: 152 kt | 175 mph | 282 kmh
VNE: 181 kt | 208 mph | 335 kmh
Empty Weight: 363 kg | 800 lbs
MTOW Weight: 646 kg | 1425 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 500 ft | 152 m
Landing distance (50ft obstacle): 600 ft | 183 m
Aircraft information: Text and photo from: http://www.arionaircraft.com
The Arion Aircraft design team cut their teeth in the amateur built light plane sector of the aviation world over the last 15 years. After progressing from Kolbs to Titans to RV's and Esquals, the vision began to emerge of a new sort of light aircraft. One that would look great and offer outstanding performance while remaining affordable for the average amateur builder. To that end four clear design goals emerged:
1. Generous Margins for Safety and Strength
2. Simplicity of Systems for Quick Easy Construction
3. High Performance per HP
4. Excellent Flying Qualities
Safety & Strength ....
The structure of the Lightning was tested extensively for symmetrical and asymmetrical flight loads to over 9 G at a gross weight of 1320 lbs. Torsional testing of the fuselage and tail, load testing of welded parts round out the strength testing profile.
Ballistic Recovery Systems Inc was brought in to help design a safe, strong recovery system for the Lightning. Our fiberglass craftsmen were able to hide the installation inside the molded skins so the good looks of the Lightning would not be changed.
Simplicity ....
Through a novel mix of molded fiberglass components and welded 4130 steel structures, Arion's team was able to engineer a construction method where no epoxy layups are needed to complete the kit. Just open the box, trim and fit the parts, complete some final fabrication of the parts and bolt the plane together. Top quality aircraft grade hardware is used throughout.
Performance....
The Lightning cruises at 175 mph on 120 hp, burning 5.5 gallons per hour. Solo climb rates settle in at 1700 fpm. Roll rates exceed 45 degrees/second. Top speed is 190 mph. Need we say more...?
Flying ....
Quick to respond, eager to turn, anxious to accelerate ... this airplane exhibits the strength, speed, and agility of its namesake; Arion, the immortal horse of Hercules. Yet control is stable, light, and intuitive. Just "think" a maneuver and it just seems to happen. In the pattern Lightning slows unbelievably well to a touchdown speed under 50 mph. Slow speed handling in the pattern is solid. It's a cool cat in the pattern but that Tiger's heart is ready to roar.
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Price: Not given
|
Stall: 34 kt | 39 mph | 63 kmh
Cruise: 103 kt | 118 mph | 190 kmh
VNE: 139 kt | 160 mph | 258 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 0 kg | 0 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Ultralight Aircraft with retractable gear - options available -
ready to fly starting of 66.000 €
visit
www.capco-aviation.be
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Price: 66000 EURO
|
Stall: 35 kt | 40 mph | 65 kmh
Cruise: 130 kt | 150 mph | 241 kmh
VNE: 143 kt | 165 mph | 265 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 550 kg | 1213 lbs
Climb Ratio: 1700 ft/min | 9 m/s
Glide Ratio: 1:17
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 660 ft | 200 m
Aircraft information: This aerodynamic, cantilevered, low wing sport pilot aircraft of mixed construction can transport two people over 800 statute miles at a maximum cruising speed of 155 mph. And it all begins with a quick 200 to 400 foot ground roll on a grass or concrete strip. Before you know it, you're in the air, rapidly accelerating toward a maximum climb rate of nearly 1,700 feet per minute!
But that's not all because, with the history behind the ATEC Zephyr, you have peace of mind.
Developed in collaboration with renowned Czech aircraft designer, Oldrich Olsansky, the ATEC Zephyr Sport Pilot airplane has an impeccable safety record since its debut over six years ago. With over 110 units plying the skies of Australia, Europe and North America, the plane is thoroughly proven and exceptional from a reliability and economic standpoint.
What's more, buyers have two paths to choose from when it comes to buying one. Sport Pilot, Amateur-built (Experimental in the U.S.) or Ultralight (Canada only; Advanced Ultralight pending). By opting for the first category, operators can enjoy all of the benefits of a fully-certified aircraft minus outrageous acquisition, operating and maintenance costs. Moreover, they can even train student pilots in a flying club environment. For those who no longer qualify for the standard aviation medical, the Ultralight and Sport Pilot categories less restrictive requirements may be the answer. Either way, one thing's sure. With an ATEC Zephyr, you no longer have to sacrifice performance and flexibility for affordability.
The MTOW is 472.5 kg in the European ultralight version and in US the LSA version of the Zephyr allows 550 kg. The LSA Zephyr is called Zephyr 2550.
Text from: http://www.atecaviation.com/
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Price: 44000 EURO
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Stall: 32 kt | 37 mph | 60 kmh
Cruise: 124 kt | 143 mph | 230 kmh
VNE: 148 kt | 171 mph | 275 kmh
Empty Weight: 275 kg | 606 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: 1:18
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 980 ft | 300 m
Aircraft information: The ATEC 321 FAETA is an aerodynamically refined cantilever low-winged all composit aircraft with a high content of carbon fibre. The ultralight modification is a basic one of the project series of very light sport planes of a derived design. Swift and manoeuvrable aircraft providing over standard comfort for a two-person crew and a safe sensation in the spacious cockpit. The low-weight but rigid airframe makes possibility equipe aircraft with a high-speed parachute rescue system without a drastic loss of payload. The adequate wing area together with an efficient slotted flap give the plane be able fly with an extremely low speed.
The WING is a reinforced shell of a carbon-fibre sandwich. The tapered backswept wing of a SM 701 airfoil along the all span. The all composite main wing spar is equipped with carbon flanges designed for a high safety factor. The high efficient slotted flap has been developed using latest methods of computer design engineering. All external details of wing like flap hinges, slots, Pitot tube attachement, wing tips have been shaped with respect for minimum air drag.
The FUSELAGE is a carbon-fibre shell braced by multi-layer wooden bulkheads. The cross-section is elliptic with pure wing fillets and a spacious cabin. The hinged perspex canopy can swing upwards and backwards. The engine which is in the front part of the fuselage is separated by the firewall, to which the engine bearer attachment and the steerable nosewheel are attached.
The TAIL UNIT all composite arranged in T-shape. The tapered horizontal tail surface with an elevator is constructed in a way similar to that of a wing. The tapered vertical tail surface is a monolithic part of the fuselage shell. The rudder suspended from the last fuselage bulkhead is completely of composites.
The LANDING GEAR is a fixed three-wheeled construction with a steerable nose wheel. The main gear is constructed as a pair of leaf springs of composites. The front leg is made of composites and metal tubes. The main wheels are equipped with disc brakes. The size of main tyres: 350x120 mm, while that of front tyre is 300x100 mm. All wheels have aerodynamic fairing.
The CONTROL. Dual control of all the rudders. The ailerons, flaps and elevator are controlled through the control rods and levers, the rudder through the steel wire ropes. All the control attachments are situated within the airframe. The important checking points in the wings are equipped with inspection holes with a perspex covering.
The ENGINE of standard option is ROTAX 912 UL 80 HP or ROTAX 912 SUL 100 HP that drives a FITI three or two blade propeller ground adjustable. The engine bed attachment is welded of the first-rate-quality CrMo steel tubes.
The FUEL SYSTEM consists of the fuel tank integrated in the fuselage and the piping connection equipped with a sediment bowl and a drain plug. The pressure of the fuel is measured by a fuel-pressure gauge.
The ISTRUMENTATION consists of basic flight, engine and navigation checking instruments. The static and dynamic pressure is taken from the Pitot tube attached below the port wing.
Text and photo from www.atecvos.cz/
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Price: Not given
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Stall: 35 kt | 40 mph | 65 kmh
Cruise: 130 kt | 149 mph | 240 kmh
VNE: 157 kt | 180 mph | 290 kmh
Empty Weight: 200 kg | 441 lbs
MTOW Weight: 300 kg | 661 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: -
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Price: Not given
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Stall: 41 kt | 47 mph | 76 kmh
Cruise: 113 kt | 130 mph | 210 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 340 kg | 750 lbs
MTOW Weight: 590 kg | 1300 lbs
Climb Ratio: 800 ft/min | 4,2 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 590 ft | 180 m
Aircraft information: Text and photo from www.aveousa.com
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Price: Not given
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Stall: 35 kt | 40 mph | 64 kmh
Cruise: 67 kt | 78 mph | 125 kmh
VNE: 100 kt | 115 mph | 185 kmh
Empty Weight: 230 kg | 507 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 825 ft/min | 4 m/s
Glide Ratio: 9/1
Take-off distance (50ft obstacle): 820 ft | 250 m
Landing distance (50ft obstacle): 920 ft | 280 m
Aircraft information: parachute GRS450
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Price: Not given
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Stall: 35 kt | 40 mph | 65 kmh
Cruise: 72 kt | 83 mph | 133 kmh
VNE: 89 kt | 103 mph | 165 kmh
Empty Weight: 215 kg | 474 lbs
MTOW Weight: 390 kg | 860 lbs
Climb Ratio: 600 ft/min | 3,85 m/s
Glide Ratio: 10,8
Take-off distance (50ft obstacle): 620 ft | 190 m
Landing distance (50ft obstacle): 1100 ft | 335 m
Aircraft information: Information from POH for SE-YMV
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Price: Not given
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Stall: 28 kt | 32 mph | 52 kmh
Cruise: 60 kt | 69 mph | 111 kmh
VNE: 86 kt | 99 mph | 159 kmh
Empty Weight: 184 kg | 406 lbs
MTOW Weight: 390 kg | 860 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 17:1
Take-off distance (50ft obstacle): 750 ft | 230 m
Landing distance (50ft obstacle): 460 ft | 140 m
Aircraft information: The Chevvron 2-32C 2 seat Microlight aircraft. Possibly the quietest production aircraft available and with an impeccable safety record. 40 sold worldwide to date. As close as you can get to a Microlight Motorglider at a fraction of the price.
Text and photo from: http://www.aviationenterprises.co.uk/avent/chevron.htm
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Price: Not given
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Stall: 45 kt | 52 mph | 83 kmh
Cruise: 137 kt | 158 mph | 254 kmh
VNE: 155 kt | 178 mph | 287 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 0 kg | 0 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 21:1
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: The Magnum is a quantum leap in light aircraft design and performance with the pedigree of full CAA Type Certification behind it which ensures the quality, back up and long life which such an aircraft demands.
FIRST - Fully CAA Type Approved.
FIRST - All composite hydraulic fully retracting tricycle undercarriage
FIRST - 30% Fowler flaps with low drag cruise setting
FIRST - 160 kts continuous cruise on 100 HP 1000 nautical miles range
FIRST - 200 kg crew, 50 kg baggage, room for skiis 21:1 L/D ratio, max 21 deg alpha
Text and photo from:
http://www.aviationenterprises.co.uk/avent/magnum.htm
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Price: Not given
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Stall: 31 kt | 36 mph | 58 kmh
Cruise: 113 kt | 130 mph | 209 kmh
VNE: 156 kt | 180 mph | 290 kmh
Empty Weight: 449 kg | 990 lbs
MTOW Weight: 794 kg | 1750 lbs
Climb Ratio: 1800 ft/min | 9 m/s
Glide Ratio: N/A
Take-off distance (50ft obstacle): 225 ft | 69 m
Landing distance (50ft obstacle): 200 ft | 61 m
Aircraft information: Different literature from Avid gives different data for the same aircraft – none is dated so it’s hard to determine what’s current what’s outdated.
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Price: Not given
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Stall: 35 kt | 40 mph | 65 kmh
Cruise: 103 kt | 118 mph | 190 kmh
VNE: 119 kt | 137 mph | 220 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1200 ft/min | 6,9 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 460 ft | 140 m
Landing distance (50ft obstacle): 520 ft | 160 m
Aircraft information: The FK12 Comet is an ultra-light two-seat aerobatic bi-plane with an attractive durable design using modern materials.
It has good flight performance with optimised laminar flow wings with 4full length ailerons (flaperons) making it highly agile with a good view.
Due to space saving design, the wings fold down in a few minutes giving it a width of only 2.42m when the wings are folded.
Despite the classical looks, this aeroplane can travel long distances at speeds of up to 200kmh; engines used are Rotax 912 or 912S of 80-100hp making this aeroplane sporting and fun.
Text and Photo from: http://www.fk12comet.flyer.co.uk
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Price: 46000 EURO
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Stall: 35 kt | 40 mph | 64 kmh
Cruise: 106 kt | 122 mph | 197 kmh
VNE: 116 kt | 134 mph | 215 kmh
Empty Weight: 257 kg | 567 lbs
MTOW Weight: 520 kg | 1146 lbs
Climb Ratio: 1500 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 570 ft | 175 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Mercedes engine in serial aircraft
Fk-Lightplanes is the first manufacturer to offer this engine system in a serial aircraft. For this purpose, a special model, the FK9 Smart was created.
This design is not just an FK9 fitted with a Mercedes Smart engine. It is rathermore a complete package embodying its own special philosophy and technology and echoing in this respect the idea of the smart automobile.
This concept uses the lightweight FK9 Utility airframe, with more sophisticated paintwork and furnishings than the basic version. The streamlined technology implemented includes practical systems and instruments; superfluous details have been deliberately excluded. Configuration and equipment are serial installations but the plane comes ready to "fly away"!
This allows a serial price that is wide below a similarly equipped Rotax FK9. All this, not to forget the significantly lower fuel consumption and much less expensive maintenance.
After all - it's "smart"...
Photo and text from: http://www.fk-lightplanes.com/html/fk9_-_mk_iv.html
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Price: Not given
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Stall: 35 kt | 40 mph | 64 kmh
Cruise: 131 kt | 151 mph | 243 kmh
VNE: 157 kt | 180 mph | 290 kmh
Empty Weight: 275 kg | 606 lbs
MTOW Weight: 520 kg | 1146 lbs
Climb Ratio: 1500 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: The FK 14 Polaris Light Plane
The fast cruiser without compromise!
In addition to its modern design, the Polaris distinguishes itself not only because of its outstanding panorama view, but also due to its low fuel consumption which in turn allows far-ranging hauls.
Text and photo from: http://www.fk-lightplanes.com/html/fk_14_polaris.html
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Price: Not given
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Stall: 32 kt | 37 mph | 60 kmh
Cruise: 70 kt | 81 mph | 130 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 230 kg | 507 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 10
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: 50 HP to 80 HP engine
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Price: 18000 USD
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Stall: 22 kt | 25 mph | 40 kmh
Cruise: 36 kt | 42 mph | 67 kmh
VNE: 49 kt | 56 mph | 90 kmh
Empty Weight: 105 kg | 231 lbs
MTOW Weight: 200 kg | 441 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 70 ft | 20 m
Landing distance (50ft obstacle): 160 ft | 50 m
Aircraft information: -
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Price: 6000 EURO
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Stall: 58 kt | 67 mph | 107 kmh
Cruise: 140 kt | 161 mph | 259 kmh
VNE: 240 kt | 276 mph | 444 kmh
Empty Weight: 450 kg | 992 lbs
MTOW Weight: 726 kg | 1600 lbs
Climb Ratio: NA ft/min | 0 m/s
Glide Ratio: NA
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Unlimited aerobatic capacity.
G-LOAD Max 10G positive or negative
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Price: Not given
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Stall: 51 kt | 59 mph | 95 kmh
Cruise: 156 kt | 180 mph | 290 kmh
VNE: 174 kt | 200 mph | 322 kmh
Empty Weight: 209 kg | 460 lbs
MTOW Weight: 376 kg | 830 lbs
Climb Ratio: 1900 ft/min | 10 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 750 ft | 229 m
Landing distance (50ft obstacle): 700 ft | 213 m
Aircraft information: The BD-5 is a high performance single-place, low-wing, pusher-configuration sport plane. Design features include all-metal construction, mechanical retractable landing gear among the industry finest, detachable wings,and wrist action side stick control as in modern day fighter aircraft. Originally developed in the early 1970s the aircraft was designed to day VFR requirements for use in sport and recreational flying, including limited aerobatic capability.
Text: http://www.bd-micro.com/
Photo: http://www.bd5.com
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Price: Not given
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Stall: 30 kt | 35 mph | 56 kmh
Cruise: 80 kt | 92 mph | 148 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 190 kg | 419 lbs
MTOW Weight: 410 kg | 904 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Text and photo from: http://www.bellaaviation.co.uk/
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Price: Not given
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Stall: 34 kt | 39 mph | 63 kmh
Cruise: 90 kt | 104 mph | 167 kmh
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