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]

3xtrim
450 ultra


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

450 ultra
Price: Not given

AAC Amfibian of Canada, LTD.
Seastar Amfibian


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.

--- 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/

Seastar Amfibian
Price: Not given

ABS AEROLIGHT
Xenon ultralight Autogyro


Stall: 22 kt | 25 mph | 40 kmh
Cruise: 139 kt | 160 mph | 257 kmh
VNE: 174 kt | 200 mph | 322 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/

Xenon ultralight Autogyro
Price: 65000 EURO

Ace Aircraft Company
Corben Baby Ace


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/

Corben Baby Ace
Price: 18950 USD

Ace Aircraft Company
Corben Junior Ace


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/

Corben Junior Ace
Price: 20950 USD

Aero Adventure Inc.
Aventura II


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.

------------------------
Editors note: Take-off and landing distance on land and not over 50ft obstacle

Text and Photo from: http://www.aeroadventureinc.com

Aventura II
Price: Not given

Aero Bravo Indústria Aeronáutica Ltda
Bravo 700


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:
-

Bravo 700
Price: Not given

Aero Services
Guepard


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:
-

Guepard
Price: Not given

Aero Services
Guépy


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

Guépy
Price: Not given

Aerocomp inc.
Merlin


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

Merlin
Price: 35995 USD

AéroConsult
Jodel D20 UL Legende


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.

Jodel D20 UL Legende
Price: Not given

Aerocopter
Futura


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/

Futura
Price: Not given

Aerodynos De Colombia S.A.
JA 177 Evolution I


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

JA 177 Evolution I
Price: Not given

Aerojames
Isatis 01


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

Isatis 01
Price: Not given

Aeromoragon S.L.
Moragon


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

Moragon
Price: 42000 EURO

Aeronix
Airelle


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

Airelle
Price: Not given

Aeroplanes DAR
DAR-21


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

DAR-21
Price: Not given

Aeroplanes DAR
DAR-23


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

DAR-23
Price: Not given

Aeroplanes DAR
DAR-21 S


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

DAR-21 S
Price: Not given

Aeroplanes DAR
SpeedSter


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.

SpeedSter
Price: 30000 EURO

Aeroprakt
A-22 Foxbat


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

A-22 Foxbat
Price: Not given

Aeropro CZ
EuroFox


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

EuroFox
Price: 39500 EURO

AEROPUP
Aeropup 2 place


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.

Aeropup 2 place
Price: 18000 USD

AeroSpool
Dynamic WT9


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

Dynamic WT9
Price: 60000 EURO

Aerostar
Festival R40S


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.

Festival R40S
Price: Not given

Aerostyle (Aerosport Ltd in US)
Breezer


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/

Breezer
Price: Not given

AEROTEC
DEKO-17


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

DEKO-17
Price: Not given

AEROTEC
DEKO - 8 VLA Club


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/

DEKO - 8 VLA Club
Price: Not given

AEROTEC
DEKO-17AT


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

DEKO-17AT
Price: Not given

Aerotrike
Safari


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!

Safari
Price: Not given

Aeroworks
Aerolite 103


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.

Aerolite 103
Price: Not given

Affordaplane Aircraft Co.
Affordaplane


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

Affordaplane
Price: 3000 USD

Aircraft Rakusan -Czech Republic
UCL Maja Ultralight


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

UCL Maja Ultralight
Price: 20 EURO

Aircraft Sales and Parts LTD (ASAP)
Chinook PLUS 2


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

Chinook PLUS 2
Price: 17995 USD

Aircraft Sales and Parts LTD (ASAP)
Chinook PLUS 2 With 582


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

Chinook PLUS 2 With 582
Price: 19995 USD

Aircraft Sales and Parts LTD (ASAP)
Chinook Plus 2 with HKS 700E


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

Chinook Plus 2 with HKS 700E
Price: 20995 USD

Aircraft Sales and Parts LTD (ASAP)
Chinook Plus 2 with Rotax 912


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

Chinook Plus 2 with Rotax 912
Price: 27500 USD

Aircraft Sales and Parts LTD (ASAP)
Summit II Powered Parachute


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

Summit II Powered Parachute
Price: 15950 USD

Aircraft Sales and Parts LTD (ASAP)
Beaver SS-single place


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

Beaver SS-single place
Price: 13150 USD

Aircraft Spruce & Specialty Co.
Wittman Tailwind


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

Wittman Tailwind
Price: Not given

Airdrome Aeroplanes
Fokker DR-1 Triplane 3/4 replica


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/

Fokker DR-1 Triplane  3/4 replica
Price: Not given

Airdrome Aeroplanes
Fokker E-III Eindecker 3/4 replica


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

Fokker E-III Eindecker 3/4 replica
Price: Not given

Airdrome Aeroplanes
Dream classic


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

Dream classic
Price: Not given

Airmax
Seamax


Stall: 31 kt | 36 mph | 58 kmh
Cruise: 113 kt | 130 mph | 209 kmh
VNE: 139 kt | 160 mph | 257 kmh
Empty Weight: 300 kg | 661 lbs
MTOW Weight: 520 kg | 1146 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 Krister Karlsmoen

amfibian LSA / Ultralight Airmax Seamax

Seamax
Price: Not given

Airsport s.r.o.
Sonet


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:
-

Sonet
Price: Not given

Airsport s.r.o.
Sonata


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.

Sonata
Price: Not given

Alisport Srl
Yuma


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.

Yuma
Price: Not given

Alpaero
Choucas


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.

Choucas
Price: Not given

Alpi Aviation
Pioneer 300


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

Pioneer 300
Price: 66000 EURO

Alpi Aviation
Pioneer 200


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

Pioneer 200
Price: 42500 EURO

Alpi Aviation
Pioneer 300


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

Pioneer 300
Price: 52000 USD

Ameri-Cana Ultralights
Eureka


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

Eureka
Price: 8000 USD

American Legend Aircraft Company
Legend Cub AL3C-100


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

Legend Cub AL3C-100
Price: Not given

Ameriplanes
Mitchell Wing A-10


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/

Mitchell Wing A-10
Price: 11700 USD

AMS Flight
Magnus AM21


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

Magnus AM21
Price: Not given

AMS Flight
Magnus AM11


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

Magnus AM11
Price: Not given

AMS Flight
Carat A


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.

Carat A
Price: Not given

Andreasson
BA-4B


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.

BA-4B
Price: Not given

Apollo Ultralight Aircraft
Apollo Fox


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).

Apollo Fox
Price: Not given

Asso Aerei
Champion V


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

Champion V
Price: 66000 EURO

Atec
Zephyr 2000 C, 2550


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/

Zephyr 2000 C, 2550
Price: 44000 EURO

Atec
321 Faeta


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/

321 Faeta
Price: Not given

Atec
212 Solo


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:
-

212 Solo
Price: Not given

Aveotech
Aveo XT


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

Aveo XT
Price: Not given

Aviasud Engineering
Albatros AE209


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

Albatros AE209
Price: Not given

Aviasud Engineering
Mistral


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

Mistral
Price: Not given

Aviation Enterprises
Chevvron 2-32C


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

Chevvron 2-32C
Price: Not given

Aviation Enterprises
Magnum VLA


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

Magnum VLA
Price: Not given

Avid Aircraft Inc.
Catalina amphibian


Stall: 38 kt | 44 mph | 70 kmh
Cruise: 63 kt | 72 mph | 117 kmh
VNE: 80 kt | 92 mph | 148 kmh
Empty Weight: 346 kg | 763 lbs
MTOW Weight: 614 kg | 1354 lbs
Climb Ratio: 450 ft/min | 2 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 500 ft | 152 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
The Avid Catalina is a three place airplane that can take-off of land or water. It's even better than amphibious floats because this airplane uses tundra tires and can taxi up on the beach.

This planes was formerly named Avid Amphibian. Text From: http://www.fmtc.com/~sos1/catalina.html

Catalina amphibian
Price: Not given

Avid Aircraft Inc.
IV


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.

IV
Price: Not given

B&F Technik Factory
FK12 Comet


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

FK12 Comet
Price: 46000 EURO

B&F Technik Factory
FK 9 Mk IV Utility


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

FK 9 Mk IV Utility
Price: Not given

B&F Technik Factory
FK14 Polaris


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 131 kt | 151 mph | 243 kmh
VNE: 157 kt | 180 mph | 290 kmh
Empty Weight: 284 kg | 626 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

FK14 Polaris
Price: Not given

BAaer
BA-5 Gurí


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

BA-5 Gurí
Price: 18000 USD

bagalini
bagaliante


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:
-

bagaliante
Price: 6000 EURO

BCT Aero,Inc
Giles G202


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

Giles G202
Price: Not given

BD Micro Technologies
BD-5B


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

BD-5B
Price: Not given

Bella Aviation
Shadow


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/

Shadow
Price: Not given

Best Off
Skyranger V MAX


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 90 kt | 104 mph | 167 kmh
VNE: 112 kt | 129 mph | 207 kmh
Empty Weight: 255 kg | 562 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 1:10
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
The SkyRanger was designed by Philippe Prevot in Toulouse, the capital of the French Aeronautical industry in the early 90’s. The aim of the design of SkyRanger was to produce a high performance microlight (a European term for ultra-light) airplane of the simplest possible construction to be assembled, inspected and repaired by anybody. Using the geometric strength of a triangle, he patented his cabin frame design. Structural studies were done by one of the most respected aeronautical schools, ENSICA, that confirmed both the strength and light weight of the craft using only straight tubes and no welding.

98 Sky Rangers were then manufactured in France from 1992 to 1997 under license by SYNAIRGIE.

The SkyRanger is today manufactured under license by Aeros LTD in the Ukraine, by ex Antonov workers, to very high standards.

600+ SkyRangers are now flying all around the world, with over 100 in the United States

Fast build kit. Photo from: http://www.skyranger.se

Skyranger V MAX
Price: Not given

Bilsam Aviation
Sky Cruiser


Stall: 43 kt | 49 mph | 79 kmh
Cruise: 113 kt | 130 mph | 209 kmh
VNE: 135 kt | 155 mph | 249 kmh
Empty Weight: 326 kg | 718 lbs
MTOW Weight: 570 kg | 1256 lbs
Climb Ratio: 1121 ft/min | 6 m/s
Glide Ratio: 15/1
Take-off distance (50ft obstacle): 935 ft | 285 m
Landing distance (50ft obstacle): 721 ft | 220 m

Aircraft information:
Bilsam Aviation is a new company that is utilizing the talant from Polish Military and Glider industry. The first aircraft being introduced is the Sky Cruiser

Sky Cruiser
Price: 69 USD

Boris Borisevic
P-200


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 67 kt | 78 mph | 125 kmh
VNE: 84 kt | 97 mph | 156 kmh
Empty Weight: 370 kg | 816 lbs
MTOW Weight: 570 kg | 1257 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 7.2
Take-off distance (50ft obstacle): 520 ft | 160 m
Landing distance (50ft obstacle): 460 ft | 140 m

Aircraft information:
Very strong airplane,steel tube fuselage aluminum covered,with all metal wings and empennage. Ballistic parachute . Contact: bb@orenavia.com

P-200
Price: 20000 USD

BRM - Construçoes Aeronauticas Lda
Land Africa - Impala


Stall: 19 kt | 22 mph | 36 kmh
Cruise: 84 kt | 96 mph | 155 kmh
VNE: 111 kt | 127 mph | 205 kmh
Empty Weight: 272 kg | 600 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:
STOL ultralight Produced in Portugal

Land Africa - Impala
Price: Not given

BRM - Construçoes Aeronauticas Lda
Land Africa - Druiker


Stall: 19 kt | 22 mph | 36 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 111 kt | 127 mph | 205 kmh
Empty Weight: 255 kg | 562 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:
STOL Ultralight Produced in Portugal

Land Africa - Druiker
Price: Not given

BRM - Construçoes Aeronauticas Lda
Land Africa - Palanca


Stall: 19 kt | 22 mph | 36 kmh
Cruise: 94 kt | 109 mph | 175 kmh
VNE: 111 kt | 127 mph | 205 kmh
Empty Weight: 275 kg | 606 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 130 ft | 40 m
Landing distance (50ft obstacle): 130 ft | 40 m

Aircraft information:
STOL ultralight Produced in Portugal

Land Africa - Palanca
Price: Not given

Brügger
Colibri MB2


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 190 kg | 419 lbs
MTOW Weight: 0 kg | 0 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Colibri MB2.

Colibri MB2
Price: Not given

Bushcaddy
R-80


Stall: 30 kt | 34 mph | 55 kmh
Cruise: 83 kt | 95 mph | 153 kmh
VNE: 113 kt | 130 mph | 209 kmh
Empty Weight: 294 kg | 648 lbs
MTOW Weight: 559 kg | 1232 lbs
Climb Ratio: 850 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Photo from http://www.bushcaddy.com/ The weights is for wheel version.

R-80
Price: Not given

CAG
Toxo ultralight


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 119 kt | 137 mph | 220 kmh
VNE: 189 kt | 217 mph | 350 kmh
Empty Weight: 284 kg | 626 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1400 ft/min | 7,5 m/s
Glide Ratio: 16
Take-off distance (50ft obstacle): 160 ft | 49 m
Landing distance (50ft obstacle): 250 ft | 76 m

Aircraft information:
CAG Toxo is available with bigger engines in VLA version.

Toxo ultralight
Price: Not given

Carlson Aircraft
Sparrow Ultralight


Stall: 23 kt | 26 mph | 42 kmh
Cruise: 50 kt | 58 mph | 93 kmh
VNE: 55 kt | 63 mph | 101 kmh
Empty Weight: 115 kg | 254 lbs
MTOW Weight: 229 kg | 504 lbs
Climb Ratio: 750 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 240 ft | 73 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
Carlson Aircraft Sparrow Ultralight

Using proven aircraft design and materials, the SPARROW ULTRALIGHT offers unprecedented reliability and true airplane performance. Not just a "wing and sling," this is a real three axis controlled aircraft conforming to FAA 103 regulations. Easy to build and fun to fly, The SPARROW ULTRALIGHT is affordable, economical and a superb performer. Most important, the SPARROW ULTRALIGHT has been designed with pilot safety our top priority.

Text and photo from: http://www.sky-tek.com/spul.html#Specifications

Sparrow Ultralight
Price: Not given

CGS Aviation
CGS Hawk Classic Two Seat


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 56 kt | 65 mph | 105 kmh
VNE: 87 kt | 100 mph | 161 kmh
Empty Weight: 179 kg | 395 lbs
MTOW Weight: 431 kg | 950 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:
CGS Hawk Classic Two Seat

The Hawk Classic Two Seat was designed for those who wanted the excellent flight and handling characteristics of our Hawk Classic Single Seat, but needed to carry a passenger or give flight instruction. The Hawk Classic Two Seat easily fits the requirements of Part 103-7 Waiver for Two Seat Instruction. With an empty weight of 395 lbs. equipped with a Rotax 503 and 440 lbs. equipped with a Rotax 582 (electric start and brakes), we are well under the weight limit of 490 lbs.

The Hawk Classic Two Seat incorporates tandem seating rather than side by side. This allows a student to feel as if he is flying in a single place during his all important instructional phase because the instructor is out of sight and behind him. When it is time to solo, the student pilot experiences more confidence and less stress with this seating arrangement. He is not suddenly dealing with an empty seat next to him. With tandem seating, turns to the left or right are equally comfortable because you don't have to look across a seat to check behind you. In addition, since most ultralight aircraft are pushers, the tandem configuration allows for better inflow to the propeller, and much less drag. Center of gravity changes are also much less pronounced when flying solo vs. with a passenger. In a tandem set up, the front pilot balances the engine, and the passenger sits on the center of gravity, so it makes no difference if you have a passenger or not. The center of gravity changes very little. In a side by side arrangement, however, when the passenger exits the plane, the center of gravity makes a drastic shift to the rear, and must be compensated for in some way.

On the Hawk Classic Two Seat the rear seat is designed to sit slightly higher than the front seat so the field of vision of the passenger or instructor in the rear seat is not obstructed. Other design features of the Hawk Classic Two Seat include: the wing design has a double surface flat bottomed airfoil for stable flight characteristics. The nose is rounded on the bottom and the windshield has a flatter angle than the CGS Hawk Arrow models. Flaps (not flaperons) are standard equipment on all Hawks and are very effective in increasing climb rate and decreasing landing distance. At the heart of the Hawk's unique design is its curved boom tube (which has never been successfully copied by any other ultralight manufacturer). The curved boom allows the horizontal stabilizer to be placed up and above the down wash of the wing, especially when flaps are deployed. Another benefit of the curve is shorter landing gear legs making it easier to get in and out of your plane. The curved boom also is stronger in torsion than a straight boom, and allows the airplane to rotate for take offs and landings in a normal fashion without banging the boom on the ground. It is also aesthetically pleasing to look at.

Photo and text from: http://www.cgsaviation.com/singleclassic.htm

CGS Hawk Classic Two Seat
Price: Not given

CGS Aviation
CGS Hawk Arrow Two Seat


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 56 kt | 65 mph | 105 kmh
VNE: 87 kt | 100 mph | 161 kmh
Empty Weight: 191 kg | 420 lbs
MTOW Weight: 431 kg | 950 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:
The Hawk Arrow series was originally designed as an updated version of the Hawk Classic, incorporating features requested over a period of years. The nose section is longer, more pointed, and angles downward (steeper) than what you find in the Hawk Classic. This allows for better forward visibility at low sun angles. The nose also has a flatter floor section. Since the nose was made longer, the area of the rudder and vertical stabilizer were increased in order to enjoy the same excellent yaw stability of the Hawk Classic. The tail boom was also reinforced to handle the loads of this larger tail assembly.

The Hawk Arrow Two Seat wing has the same semi symmetrical airfoil as the Hawk Sport, and streamlined extruded aluminum wing struts. Standard features of the Hawk Arrow also include curved overhead and curved windshield. This model is for those who like the more modern jet plane look, yet still want the excellent flying characteristics of the Hawk Classic. Primarily it’s a personal preference, some folks seem to like the smoother rounder lines of the Classic while others like the more modern jet plane look of the Arrow. Either way they all have the same excellent flying characteristics.

The Hawk Arrow Two Seat incorporates tandem seating rather than side by side. This allows a student to feel as if he is flying in a single place during his all important instructional phase because the instructor is out of sight and behind him. When it is time to solo, the student pilot experiences more confidence and less stress with this seating arrangement. He is not suddenly dealing with an empty seat next to him. With tandem seating, turns to the left or right are equally comfortable because you don\'t have to look across a seat to check behind you. In addition, since most ultralight aircraft are pushers, the tandem configuration allows for better inflow to the propeller, and much less drag. Center of gravity changes are also much less pronounced when flying solo vs. with a passenger. In a tandem set up, the front pilot balances the engine, and the passenger sits on the center of gravity, so it makes no difference if you have a passenger or not. The center of gravity changes very little. In a side by side arrangement, however, when the passenger exits the plane, the center of gravity makes a drastic shift to the rear, and must be compensated for in some way.

On the Hawk Arrow Two Seat the rear seat is designed to sit slightly higher than the front seat so the field of vision of the passenger or instructor in the rear seat is not obstructed. Flaps (not flaperons) are standard equipment on all Hawks and are very effective in increasing climb rate and decreasing landing distance. At the heart of the Hawk\'s unique design is its curved boom tube (which has never been successfully copied by any other ultralight manufacturer). The curved boom allows the horizontal stabilizer to be placed up and above the down wash of the wing, especially when flaps are deployed. Another benefit of the curve is shorter landing gear legs making it easier to get in and out of your plane. The curved boom also is stronger in torsion than a straight boom, and allows the airplane to rotate for take offs and landings in a normal fashion without banging the boom on the ground. It is also aesthetically pleasing to look at.

Photo and text from: http://www.cgsaviation.com/twoplacearrow.htm

CGS Hawk Arrow Two Seat
Price: Not given

Colyaer s.l.
Gannet S100


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 97 kt | 112 mph | 180 kmh
VNE: 140 kt | 162 mph | 260 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 20
Take-off distance (50ft obstacle): 140 ft | 43 m
Landing distance (50ft obstacle): 140 ft | 43 m

Aircraft information:
Amfibian Ultralight!

The Colyaer Gannet S100 is a seaplane that shares the wing, tail and upper fuselage of the Colyaer Martin 3. It has a water rudder and an optional reversible prop. On both airplanes, the engine is in the rear, which means less noise and greater visibility.

Both the Colyaer Martin 3 and the Colyaer Gannet S-100 are made of Kevlar, which has a better strength-to-weight ratio than fiberglass, making the airplane both strong and light. The airplanes will arrive 49 percent complete at Smith's shop at Pryor Field Regional Airport, also an aircraft maintenance facility.

Gannet S100
Price: Not given

Colyaer s.l.
Martin3 S100


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 97 kt | 112 mph | 180 kmh
VNE: 140 kt | 162 mph | 260 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 23
Take-off distance (50ft obstacle): 390 ft | 120 m
Landing distance (50ft obstacle): 390 ft | 120 m

Aircraft information:
Ultralight Motorglider also with shorter wingspan model 110 with better cruise = 200km/h

Martin3 S100
Price: Not given

Comco Ikarus
C-42


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 259 kg | 572 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 1:11 @ 70kn
Take-off distance (50ft obstacle): 1050 ft | 320 m
Landing distance (50ft obstacle): 770 ft | 234 m

Aircraft information:
Known as Aerosport Ltd Ikarus C42 in the US. Ikarus C42 is a popular school plane and has very nice characterics. The new model is the Ikarus C42B (C-42B)

More from: http://www.comco-ikarus.de/index_english.html

C42 - the bestseller, meanwhile more than 650 airplanes delivered worldwide -the bestselling ultralight aircraft in Germany

Maximum fun of flying at a reasonable ratio between price and performance. An innovative, modern two-seater micro-light aircraft sets the standards. The classic advantages of the ultralight and the standard aircraft categories are combined to produce a fascinating, technically matured machine. The IKARUS C 42 is thus able to fulfil expectations which were incompatible in the past: Standard aircraft comfort for the price of an ultralight. Convincing flight characteristics, safe handling and minimal parking space needed because of wings easy to remove. The C42-B will also convince you. Try it out.

www.comco-ikarus.de Photo: Tom Svensson (Pilotmagazinet.se)

C-42
Price: 40000 EURO

Comco Ikarus
C-22 Fox


Stall: 23 kt | 27 mph | 43 kmh
Cruise: 49 kt | 56 mph | 90 kmh
VNE: 65 kt | 75 mph | 120 kmh
Empty Weight: 204 kg | 450 lbs
MTOW Weight: 390 kg | 860 lbs
Climb Ratio: 700 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
-

C-22 Fox
Price: Not given

Corvus Aircraft
Corone Mk. I


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 119 kt | 137 mph | 220 kmh
VNE: 143 kt | 165 mph | 265 kmh
Empty Weight: 320 kg | 705 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 1600 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 950 ft | 290 m
Landing distance (50ft obstacle): 1050 ft | 320 m

Aircraft information:
Photo by Zoltan Mudri

Text from: http://www.corvus-aircraft.com/

The main aspect of comtructing Corvus Corone aircraft was to create a spacious, economic. twoseater light sport aircraft using high-tech composite technology. Primarily it is designed for longdistance crss-country flight and towing gliders.

The design of Corone is traditionai with the engine in the front and with nose-wheel. The fuselage is made with kevlar honeycomb sandwich structure containing carbon and glass fibre soaked with epoxy resin. This method of construction guarantees the highest possible solidity and at the same time. the lowest specific weight. The applied carbon fibre of high modulus has higher tensile strength than steel and weighs less than aluminium. All the elements of the fuselage are produced with vacuum technology using pre-preg textile and patterns.

The low position cantilever semimonocoque wings consist of two parts. The required torsion stiffness is provided by the wing skin panels. The Frise ailerons and the slotted trailing edge flaps provide for outstanding performance. The removable fuel tanks are placed in the wings.

The horizontal and vertical fin, the ailerons, the flaps, the rudder and the elevator are of pure monocoque structure. The nose wheel can be controlled with the rudder pedals. The pedals can be adjusted to the size of the pilot. The two pilots are seated side by side in the cabin. Both seats are equipped with 4 attachpoint seat belts. Corone can be controlled from either seat. The throttle, the mechanical or electronic flap and elevator trim control are on the central console. The main gear differential breaks can be operated by tilting the pedals. The sport or De-Iuxe canopy actuated with electric motor or gas-telescope opens forward.

In pieces the Corone can be stored even in a garage. It is easy to remove the wings and the horizontal stabilizator. The pilot can make the daily maintenance and operation doesn't need well equipped permanent airport.

The computer which is located at the middle of the instrument panel collects all the engine and flight parameters and shows them on an LCD monitor. In case of emergency the computer gives light and audio alert signals. The Corone can be equipped with analog instruments too.

Corone Mk. I
Price: Not given

Cri-Cri
MC-10 Cri-Cri


Stall: 39 kt | 45 mph | 72 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 159 kt | 183 mph | 295 kmh
Empty Weight: 80 kg | 176 lbs
MTOW Weight: 170 kg | 375 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 101 m
Landing distance (50ft obstacle): 495 ft | 151 m

Aircraft information:
It was in 1971, when aircraft designer Michel Colomban started work on this small aircraft Cri Cri with two engines. His target was to build small, economis plane with two engines, which would be able to flying also some aerobatic maneuvers. Price of this plane shouldn't exceed 1000 USD, including two engines - these prises are from 1970, of course:-). Constructional works took around 1500 working hours, and than was Cri-Cri plane, which name is after nickname of Michel's daughter, prepared for it's first flight.

Text from: http://flight.cz/cricri/english/index.php

MC-10 Cri-Cri
Price: Not given

CSN
Corby Starlet


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 113 kt | 130 mph | 209 kmh
VNE: 139 kt | 160 mph | 257 kmh
Empty Weight: 227 kg | 500 lbs
MTOW Weight: 340 kg | 750 lbs
Climb Ratio: 1100 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 350 ft | 107 m
Landing distance (50ft obstacle): 450 ft | 137 m

Aircraft information:
The performance of the Starlet will vary from airplane to airplane. The factors can be all up weight, engine size or horsepower, prop, or how straight the airframe was built and finished. Most of the performance figures given are for a 60 hp engine. Some Starlets have been outfitted with 2180's (75-80 hp) and these cruise at VNE (185) and climb at 1900 fpm.

The photo and text from: http://members.shaw.ca/kingdws/frameset.html

Corby Starlet
Price: Not given

Cubcrafters
CC11-100 Sport Cub


Stall: 31 kt | 36 mph | 58 kmh
Cruise: 96 kt | 110 mph | 177 kmh
VNE: 120 kt | 138 mph | 222 kmh
Empty Weight: 374 kg | 825 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 400 ft | 122 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
CERTIFICATION Text and photo from: www.cubcrafters.com

ASTM International Designation 2245:

Standard Specification for Design and Performance of a Light Sport Airplane

CC11-100 Sport Cub
Price: Not given

Czech Aircraft Works, s.r.o. (CZAW)
Zenair CH701 Stol


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 263 kg | 580 lbs
MTOW Weight: 500 kg | 1102 lbs
Climb Ratio: 1600 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 45 ft | 14 m
Landing distance (50ft obstacle): 80 ft | 24 m

Aircraft information:
Photo from: http://www.archaid.se/ultralight/planen.htm

Option: Floats

Note: landing & take-off distance is not over 50ft obstacle

Zenair CH701 Stol
Price: Not given

Czech Aircraft Works, s.r.o. (CZAW)
Zenair CH601 Zodiac


Stall: 36 kt | 41 mph | 66 kmh
Cruise: 104 kt | 120 mph | 193 kmh
VNE: 130 kt | 150 mph | 241 kmh
Empty Weight: 250 kg | 551 lbs
MTOW Weight: 480 kg | 1058 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 430 ft | 131 m
Landing distance (50ft obstacle): 550 ft | 168 m

Aircraft information:
Photo from http://www.airplane.cz/ Buy as QBK, 49% Kit or ready-to-fly

Zenair CH601 Zodiac
Price: Not given

Czech Aircraft Works, s.r.o. (CZAW)
Lake Sport Mermaid


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 100 kt | 115 mph | 185 kmh
VNE: 115 kt | 132 mph | 212 kmh
Empty Weight: 330 kg | 727 lbs
MTOW Weight: 560 kg | 1235 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 600 ft | 183 m
Landing distance (50ft obstacle): 600 ft | 183 m

Aircraft information:
Lake Sport Mermaid

The all-new Mermaid is the first amphibian to be designed especially to comply with the FAA’s new Light Sport Aircraft rules. It is also the first new certified single-engine amphibian to reach production in decades.

The design parameters were challenging: make a certifiable, roomy amphibian that will fit the LSA rules (2-place, 1235 pounds gross, low stall speed), and that will be affordable, reliable, and fun to fly; then give it the speed and range to be practical as a transportation device, and dual controls, for training and peace of mind. The Mermaid does it all, and more.

Of conventional all-metal design, the Mermaid is built by European craftsmen, with US-sourced materials. Its five watertight compartments are built with EDO-style pump-outs. The slipper-clutch Rotax 912ULS (914 also available) puts out 100 reliable horsepower while burning well under 5 gph. The useful load is over 500 pounds, and the large baggage area is located nearly on the CG, to make its capacity truly usable. The wide cockpit is comfortable; and it affords a large panel area.

Text and photo from: http://www.czaw.cz/pages/mermaid.htm

Lake Sport Mermaid
Price: Not given

Czech Aircraft Works, s.r.o. (CZAW)
Parrot


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 113 kt | 130 mph | 209 kmh
VNE: 137 kt | 157 mph | 253 kmh
Empty Weight: 360 kg | 793 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 750 ft | 229 m
Landing distance (50ft obstacle): 400 ft | 122 m

Aircraft information:
Text and photo from www.sportaircraftworks.com

The all-metal Parrot is the first LSA to offer a full-cantilever metal wing, a ‘glass’ shape in real metal, a forward-hinged canopy, and plenty of payload. Flight tests on the new machine have exceeded expectations. Test pilot and CZAW President Chip Erwin said, “I have never felt so comfortable so quickly flying any aircraft, especially a new design on its first flight. The handling and control balance are great. The visibility is fantastic. The Parrot is smooth, quiet, and extremely comfortable.” OK – he’s the company president, but others are lining up around the block to see for themselves. The entire design effort was built around the Sport Pilot (LSA) rules. “We are not adapting some 450kg European ultralight,” Erwin, born and raised in Wisconsin, explained. “We designed from the ground up for the American rules and the American market; and we use American-sourced materials. We have a new and modern look, fantastic handing characteristics on the ground and in the air, and optimized performance to the LSA rules.” With exceptionally nimble, yet steady air manners and fabulous visibility enhanced by the cantilevered wing and convenient forward-hinged canopy, the Parrot makes the most of aerodynamics. (Its efficient airfoil, developed on high-performance sailplanes, is a key feature unmatched in the industry.) The smooth shape, made possible by the Parrot’s proprietary construction fixtures, also contributes to the quiet ride. Plus, it’s beautiful. With a shape usually considered achievable only on composite aircraft, the Parrot’s stretch formed and hydroformed panels blend together with flush rivets to give the appearance of composite, without the headaches. Future headaches are also reduced by standard full-interior zinc chromate protection on the ready-to-fly machine.

Parrot
Price: Not given

Czech Aircraft Works, s.r.o. (CZAW)
SportCruiser


Stall: 30 kt | 34 mph | 55 kmh
Cruise: 117 kt | 135 mph | 217 kmh
VNE: 139 kt | 160 mph | 258 kmh
Empty Weight: 306 kg | 675 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 700 ft | 213 m
Landing distance (50ft obstacle): 400 ft | 122 m

Aircraft information:
Text and photo from: www.sportaircraftworks.com Competence and Convenience: The pilot can be ready to fly in short order, and the airplane definitely is. Sporting fantastic visibility, the all-metal, low-wing, 100hp SportCruiser is ready to take a large payload a long way, on just a little money. With pricing set at $65,000 (FOB Indiantown) and burning around 4~4.5 gallons of auto gas per hour, the SportCruiser won’t break the budget; and with its American-designed, all-metal traditional construction and US-sourced materials and airframe components, keeping it flying (and insured!) will be trouble-free. All three SAW aircraft are designed to be easy to fly, with touchdown speeds in the high 20-knot range. Sport Aircraft Works, importer and distributor of the Czech Aircraft Works designs, completed all the certification work on time. “We said in January’s announcement that we would be certified in March, and we did it,” a happy Defelici said. “It helped that we have such great support from CZAW, and that we’re learning what it takes to certify. The FAA has been great in getting this done.”

SportCruiser
Price: Not given

Czech Aircraft Works, s.r.o. (CZAW)
Zenair CH-601 XL


Stall: 38 kt | 44 mph | 70 kmh
Cruise: 120 kt | 138 mph | 222 kmh
VNE: 140 kt | 161 mph | 259 kmh
Empty Weight: 312 kg | 688 lbs
MTOW Weight: 590 kg | 1301 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 1:12
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
taildrager Factory build : 2004 Stock / new demo plane 95 hours Color : Metallic Blue / White Blue alcantara upholstery Interior -deluxe- with upholstered glovebox Engine: Rotax 912ULS 100Hp Full RCA basic 6 instruments (tso\'d) Garmin GNC 250XL panel mount radio/transponder (tso\'d) King transponder (tso\'d) Inflight adjustable prop: cruises 120-140 knots !! Whelen nav/strobe + tail light Double leading edge landing lights ( 200W ) Cigaret lighter 12V Wheel covers Cabin heat Naca air vents Locking canopy Wing bagage lockers Parking brake Electric elevator trim Electric aileron trim Electric flaps Has Now Dutch experimental registration ( PH-ZEN ) (No parachute)

Zenair CH-601 XL
Price: 64000 EURO

DAKOMAT, Poland
DEKO-5


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 57 kt | 65 mph | 105 kmh
VNE: 86 kt | 99 mph | 160 kmh
Empty Weight: 250 kg | 551 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: 6:1
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 460 ft | 140 m

Aircraft information:
DEKO-5 was designed by Polish aeronautical engineers: Marek Debski, Krzysztof Kotlinski, Type: Side-by-side ultra-light, training and observation aircraft - ideal for recreational flyer. First flight, June 1996 Design Features: Pod-and-boom fuselage. Wings braced by V-type struts. Structure: Wing and elevator are made of aluminum tubes and dacron (or ceconite) soft skin. Fuselage structure is construction, as space truss of aluminum tubes with composite joints (Polish Patent). Tail boom is made of two aluminum tubes. Cockpit canopy is made of glassfibre laminate and organic glass. The open cabin offers a very good view. The DEKO-5 is designed to a +4g / -2g load limit Power Plant: One Rotax 582 (65 hp, electric start and brakes), piston engine with reductor gear 2.58. Propeller: Junkers three-blade, carbon fibre, ground-adjustable pitch propeller. System: Ballistic parachute recovery system More info: http://www.dkd1970.webpark.pl/ Contact: dedal@ilot.edu.pl

DEKO-5
Price: Not given

Dallach
Fascination D4 BK


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 146 kt | 168 mph | 270 kmh
VNE: 157 kt | 180 mph | 290 kmh
Empty Weight: 290 kg | 639 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1600 ft/min | 8,5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Wolfgang Dallach developed not only the Sunrise and Sunwheel but also the Fascination. The Fascination is produced by W.D. Flugzeug Leichtbau GmbH from Heubach, Germany. It is powered by a Rotax 912 UL or Rotax 912 ULS engine.

Note: more information at: http://www.dallach.de

Fascination D4 BK
Price: 84000 EURO

Dallach
Evolution


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 146 kt | 168 mph | 270 kmh
VNE: 162 kt | 186 mph | 300 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1200 ft/min | 6,5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 330 ft | 100 m

Aircraft information:
Landing and takeoff is ground roll. Empty weight inkludes BRS installation! Price configurator see http://www.cal-aviation.com/ or www.dallach.de

Evolution
Price: 100 EURO

Dart Industries
Dragonfly


Stall: 58 kt | 67 mph | 107 kmh
Cruise: 145 kt | 167 mph | 269 kmh
VNE: 200 kt | 230 mph | 370 kmh
Empty Weight: 370 kg | 815 lbs
MTOW Weight: 551 kg | 1215 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Kit build, Photo from http://www.dart-industries.com/

Dragonfly
Price: Not given

Dewald Light Aircraft
Sunny


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 65 kt | 75 mph | 120 kmh
VNE: 76 kt | 87 mph | 140 kmh
Empty Weight: 190 kg | 419 lbs
MTOW Weight: 400 kg | 882 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 110 ft | 35 m
Landing distance (50ft obstacle): 180 ft | 55 m

Aircraft information:
Die SUNNY ist ein ungewöhnliches und vor allem außergewöhnliches Flugzeug. Es besitzt eine polarisierende Optik und daher gibt es Leute denen die SUNNY sofort gefällt, andere lehnen das Erscheinungsbild kategorisch ab. Dabei sind seine Stärken als offener FUN-Flieger unübertroffen.

Der Slogan "Fliegen wie ein 3-Achser, mit dem Feeling eines Trikes!" beschreibt sehr gut das Fluggefühl, den Komfort und die Sicherheit einer SUNNY. Spazierflüge bei schönem Wetter sind in diesem Flugzeug ein wahrer Genuß. Nicht umsonst verbucht der Typ steigende Absatzzahlen in wärmeren Regionen, z.B. Réunion.

Photo from: http://www.dewald-leichtflugzeugbau.de

Note: Take-off and Landing distance not over 15m obstacle.

Sunny
Price: 13499 EURO

Dewald Light Aircraft
Skyboy


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 89 kt | 103 mph | 165 kmh
Empty Weight: 268 kg | 591 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 230 ft | 70 m

Aircraft information:
Photo from: http://www.dewald-leichtflugzeugbau.de

Note: Take-off and Landing distance not over 15m obstacle.

Skyboy
Price: Not given

Direct Fly
Alto


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 285 kg | 628 lbs
MTOW Weight: 475 kg | 1047 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 440 ft | 135 m
Landing distance (50ft obstacle): 490 ft | 150 m

Aircraft information:
tailwheel or tricycle configuration

Alto
Price: 44000 EURO

Dova Aircraft
Skylark


Stall: 36 kt | 42 mph | 68 kmh
Cruise: 117 kt | 135 mph | 217 kmh
VNE: 156 kt | 179 mph | 288 kmh
Empty Weight: 296 kg | 653 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 500 ft | 152 m
Landing distance (50ft obstacle): 530 ft | 162 m

Aircraft information:
Text and photo from http://www.sportsplanes.com/

The Skylark takes Light Sport Aircraft to a new level in style. The lines and contours exude a sense of high energy and grace that not only looks good, but turns heads and delivers in performance. This two place, side-by-side, all metal, low wing aircraft provides strength and ruggedness not found in most LSA's: it can withstand 7 G's and has a Vne of 179 mph and a maximum LSA cruise of 138 MPH.

Skylark
Price: Not given

DTA
Voyageur


Stall: 28 kt | 32 mph | 52 kmh
Cruise: 54 kt | 62 mph | 100 kmh
VNE: 86 kt | 99 mph | 160 kmh
Empty Weight: 200 kg | 441 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:
The design and manufacture of the Voyageur trike is rooted in toughness and durability. Designed from the start to be much more capable than your average trike, this machine is stronger, more capable in rough conditions and more versatile than just about every machine flying today.

Voyageur
Price: Not given

DTA
Feeling


Stall: 28 kt | 32 mph | 52 kmh
Cruise: 54 kt | 62 mph | 100 kmh
VNE: 86 kt | 99 mph | 160 kmh
Empty Weight: 200 kg | 441 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 8
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
DTA is now one of the top 3 trike manufacturers in France, but a leader in the specialised touring trike segment of the market.

Feeling
Price: Not given

DTA
Combo


Stall: 27 kt | 31 mph | 50 kmh
Cruise: 54 kt | 62 mph | 100 kmh
VNE: 86 kt | 99 mph | 160 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 0 kg | 0 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 8
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
DTA’s new Combo trike puts the ‘beef’ back into ‘basic’. Available with the Rotax 503 and 582 as well as the Rotax 912 and 912S, this machine gives you performance capabilities and robust strength not normally found in an affordable and easy to inspect/maintain aircraft. With the available option of the Voyageur-II’s cantilever mast, this machine can be flown with no front strut, just like its big brother DTA Voyageur.

Combo
Price: Not given

DynAero
MCR-01 ULC Ban-Bi


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 146 kt | 168 mph | 270 kmh
VNE: 160 kt | 184 mph | 296 kmh
Empty Weight: 250 kg | 551 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 540 ft | 165 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
The MCR range of aircraft is a result of 20 years research and development by Michel Colomban and the modern manufacturing techniques developed by Dyn\\\' Aéro. Michel Colomban was for many years an engineer and aerodynamicist and was associated with Morane-Saulnier, Potez and Aerospatiale, he later designed the now famous single seat twin engine Cricri, recently of jet powered notoriety.

Text and Photo from: http://www.avnet.co.uk/lts/pages/ulc.htm

MCR-01 ULC Ban-Bi
Price: 33804 EURO

DynAero
MCR 4S


Stall: 45 kt | 52 mph | 83 kmh
Cruise: 131 kt | 151 mph | 243 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 300 kg | 661 lbs
MTOW Weight: 750 kg | 1653 lbs
Climb Ratio: 750 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 1480 ft | 450 m
Landing distance (50ft obstacle): 1800 ft | 550 m

Aircraft information:
The objective was to develop, what most thought impossible at that time:

" A four seat airplane with STOL performance, equipped with a light 100 HP engine"

The 4-S maiden flight was in June 2000.

The MCR 4-S is the only airplane in the aviation world to provide pilots with such an amazing Performance/Economy ratio. Its concept makes it to be the perfect travel aircraft, able to fly comfortably with four people onboard, cruising at more than 250 km/h, and burning only 20 L/h with a 100 hp engine. Those performances can only be reached because of the MCR 4-S very light empty weight . The aircraft can carry up to 150% of its own empty weight!

The research of a very elaborated aerodynamic design, with wing-tips optimized in wind-tunnel, and high efficiency double slotted flaps, provide the MCR 4-S with amazing STOL performances Designed around a roomy cockpit ; 1,20m width at the rear seats, build to allow four people up to 1,95m tall to be easily seated in the airplane.

The aircraft is equipped with a very strong oil-pneumatic undercarriage, allowing landings on any type of runways.

The MCR-4S can be equipped with a choice of different power plants, but may also be fitted with other options such as :

* Ballistic Recovery System parachute(actually in development)

* Extended range fuel tanks

* Toe operated Hydraulic brakes

The MCR-4S is available in kit form in respect with the CNSK regulation (specific kit airworthiness certificate) or in the "experimental" category ,depending on the registration country.

Text and photo from www.dynaero.com

MCR 4S
Price: Not given

DynAero
MCR-01 Sportster VLA


Stall: 47 kt | 54 mph | 87 kmh
Cruise: 159 kt | 183 mph | 295 kmh
VNE: 173 kt | 199 mph | 320 kmh
Empty Weight: 260 kg | 573 lbs
MTOW Weight: 490 kg | 1080 lbs
Climb Ratio: 1750 ft/min | 9 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 980 ft | 300 m

Aircraft information:
MCR 01 Sportster VLA

The initial design program started in early 1994, and the Sportster flew for the first time in July 1996

The MCR Sportster is a side by side two-seater airplane with incredible performance and capability. Fast and agile, the VLA was specially designed to reach top speed while providing the most enjoyable experience to pilots.

The MCR Sportster is a very high performance aircraft, that can cruise as fast as 300 km/h with only a 100 hp engine, at very low cost. Thanks to the highest level of technology available, and very light material, the Sportster has a very efficient direct control system that guarantees the same satisfaction as flying a fighter jet.

The MCR Sportster can be equipped with a choice of different power plants, but may also be fitted with other options such as :

* Ballistic Recovery System parachute

* Extended range wing tanks.

* Toe operated Hydraulic brakes

The MCR Sportster is available in kit form in respect with the CNSK regulation (specific kit airworthiness certificate) or in the "experimental" category depending on the registration country.

Tex and photo from: http://www.dynaero.com/lien/mcrvlauk.htm

MCR-01 Sportster VLA
Price: Not given

DynAero
MCR Pick-up


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 135 kt | 155 mph | 250 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 260 kg | 573 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 1250 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 240 ft | 73 m
Landing distance (50ft obstacle): 350 ft | 107 m

Aircraft information:
Photo from www.dynaero.com The MCR PickUp is a two seater version of the MCR 4S with a large trunk instead of the rear seats.

MCR Pick-up
Price: Not given

Earthstar Aircraft
Gull 2000


Stall: 23 kt | 27 mph | 43 kmh
Cruise: 55 kt | 63 mph | 101 kmh
VNE: 55 kt | 63 mph | 101 kmh
Empty Weight: 112 kg | 248 lbs
MTOW Weight: 249 kg | 550 lbs
Climb Ratio: 700 ft/min | 4 m/s
Glide Ratio: 12:1
Take-off distance (50ft obstacle): 250 ft | 76 m
Landing distance (50ft obstacle): 200 ft | 61 m

Aircraft information:
Considerable care has been taken in the design and testing process. The result is a stall and spin resistant aircraft with superior handling qualities both on the ground and in the air. The responsive ailerons provide roll control throughout a stall attempt. The beginning flyer will find an easy to fly, stable, and forgiving aircraft.

The Thunder Gull 2000 and Odyssey models maintain the responsive and nimble control necessary for the demanding pilot. All of the Earthstar Aircraft models are fun cross-country machines and have been flown from coast-to-coast many times.

Flight tested to a “G” loading of +5.9 and -3 and are designed to +6 and -4 yield. The ultralight model has been certified to meet the FAA’s FAR-103 requirements. VNE for all models is 120 mph.

Options include engine, instruments, propeller, side windows, parachute and others upon request.

Available as a kit or ready to fly.

All kits can be registered Experimental.

Text and photo from: http://www.thundergull.com/

Gull 2000
Price: Not given

Earthstar Aircraft
Odyssey


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 76 kt | 87 mph | 140 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 209 kg | 460 lbs
MTOW Weight: 454 kg | 1000 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: 11:1
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 175 ft | 53 m

Aircraft information:
The Thunder Gull 2000 and Odyssey models maintain the responsive and nimble control necessary for the demanding pilot. All of the Earthstar Aircraft models are fun cross-country machines and have been flown from coast-to-coast many times.

Flight tested to a “G” loading of +5.9 and -3 and are designed to +6 and -4 yield. The ultralight model has been certified to meet the FAA’s FAR-103 requirements. VNE for all models is 120 mph.

Options include engine, instruments, propeller, side windows, parachute and others upon request.

Available as a kit or ready to fly.

All kits can be registered Experimental.

Text and photo from: http://www.thundergull.com/

Odyssey
Price: Not given

EEL Homebuilt
ULF-2


Stall: 24 kt | 28 mph | 45 kmh
Cruise: 65 kt | 75 mph | 120 kmh
VNE: 76 kt | 87 mph | 140 kmh
Empty Weight: 205 kg | 452 lbs
MTOW Weight: 325 kg | 717 lbs
Climb Ratio: 600 ft/min | 3,0 m/s
Glide Ratio: 17
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 330 ft | 100 m

Aircraft information:
Only technical plans available. Approx. 3000 hours to build.

ULF-2
Price: 15000 EURO

EKOLOT
JK-05 Junior


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 97 kt | 112 mph | 180 kmh
Empty Weight: 280 kg | 617 lbs
MTOW Weight: 480 kg | 1058 lbs
Climb Ratio: 1200 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:
Contact in Poland: 0048 1343 688 97

JK-05 Junior
Price: 35000 EURO

Elam
Eurocub MK IV


Stall: 32 kt | 37 mph | 59 kmh
Cruise: 85 kt | 98 mph | 157 kmh
VNE: 110 kt | 127 mph | 204 kmh
Empty Weight: 269 kg | 593 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 1:11
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 330 ft | 100 m

Aircraft information:
Elam Eurocub has larger tail fin and elevator than the older Cuby and that gives some few knots lower stall speed.

Eurocub MK IV
Price: Not given

Euro Ala s.r.l.
Jet Fox


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 83 kt | 96 mph | 154 kmh
VNE: 97 kt | 112 mph | 180 kmh
Empty Weight: 279 kg | 616 lbs
MTOW Weight: 449 kg | 990 lbs
Climb Ratio: 1380 ft/min | 7 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 394 ft | 120 m
Landing distance (50ft obstacle): 394 ft | 120 m

Aircraft information:
stylish, comfortable cabin cabin with excellent visibility, stable & forgiving flight characteristics, aerodynamic airframe with high structural intergrity, low operational costs. Also available in handicapped version

Jet Fox
Price: 41000 EURO

Europa Aircraft
Europa Motorglider / TMG


Stall: 42 kt | 48 mph | 78 kmh
Cruise: 104 kt | 120 mph | 193 kmh
VNE: 127 kt | 146 mph | 235 kmh
Empty Weight: 358 kg | 789 lbs
MTOW Weight: 635 kg | 1400 lbs
Climb Ratio: 1100 ft/min | 5.6 m/s
Glide Ratio: 27:1
Take-off distance (50ft obstacle): 1310 ft | 400 m
Landing distance (50ft obstacle): 1310 ft | 400 m

Aircraft information:
Shaw Europa

Available as kit. Monowheel or tri-gear.

Read more in Today's Pilot: http://www.todayspilot.co.uk/flight_tests/jul02/1p1.html

Europa Motorglider / TMG
Price: Not given

Evans
Volksplane VP-1


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 70 kt | 81 mph | 130 kmh
VNE: 100 kt | 115 mph | 185 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 340 kg | 750 lbs
Climb Ratio: 200 ft/min | 1 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 1310 ft | 400 m
Landing distance (50ft obstacle): 980 ft | 300 m

Aircraft information:
The VP 1 is perhaps the simplest, least expensive wood aircraft you can build. Today there is a VP1 flying in practically every country on the globe.

Volksplane plans available from: http://www.volksplane.com/

Volksplane VP-1
Price: Not given

Evektor Aerotechnik
Eurostar / SportStar


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 113 kt | 130 mph | 210 kmh
VNE: 132 kt | 152 mph | 245 kmh
Empty Weight: 268 kg | 591 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: 1:12
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
Photo by Krister Karlsmoen

The Evektor EV-97 Team Eurostar is an ultralight aircraft designed for sport/leisure flying, touring and training with limitation to non-aerobatic VFR operations.

The Eurostar is aerodynamically controlled, single-engine, two-seat, low-wing, all metal plane with a fixed tricycle undercarriage and controllable nose wheel. The aircraft is equipped with four cylinder four stroke 80 HP Rotax 912 UL engine, optionally 100 HP Rotax 912 ULS or 80 HP Jabiru 2200.

Excellent flight features, top quality and reliability, outstanding design and high performance - these are synonyms for Team Eurostar - one of the most popular ultralight aircraft today. Today already around 400 Eurostars are flying in more than 30 countries all around the world. This aircraft is called SportStar in US and EuroStar in Europe.

Text from http://www.evektor.cz/at/en/eurostar-popis-en.html

Eurostar / SportStar
Price: 50000 EURO

EVGENIJ KOVALENKO
E-12n


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 43 kt | 50 mph | 80 kmh
VNE: 67 kt | 78 mph | 125 kmh
Empty Weight: 55 kg | 121 lbs
MTOW Weight: 145 kg | 320 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 7
Take-off distance (50ft obstacle): 480 ft | 145 m
Landing distance (50ft obstacle): 390 ft | 120 m

Aircraft information:
Very simple REAL Ultralight Aircraft for flyweight pilots. Delivered as kit package or ready to fly planes by Evgenij Kovalenko with several engine choices.

E-12n
Price: 6200 EURO

Excalibur
Excalibur Stretch


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 70 kt | 80 mph | 129 kmh
VNE: 87 kt | 100 mph | 161 kmh
Empty Weight: 204 kg | 450 lbs
MTOW Weight: 454 kg | 1000 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 11:1
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
Options include: 60-hp HKS 700E air-cooled 4-stroke or 4O-hp Rotax 447 air- cooled 2-stroke engine, instruments (ASI, altimeter, tach, dual CHT dual EGT, panel-mounted compass, ignition switch), standard or amphibious floats, fiberglass wheel pants, BRS ballstic emergency parachute, doors, strobe lights and paint materials.

Construction is 6061-T6 and 2024-T3 aluminum tube airframe with chromoly steel weldments where needed, stainless steel pop rivets and AN or military spec hardware. Wings and surfaces are covered with Superflite fabric. No welding or machining is necessary and all the critical work is completed at the factory.

The kit for the Excalibur II features prebuilt tail surfaces, wings, ailerons end fuselage, and all the controls are already installed. Build time for the kit is estimated at 100 to 200 hours.

Text and photo from: http://www.excaliburaircraft.com

Excalibur Stretch
Price: Not given

Fantasy Air
Allegro 2000


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 119 kt | 137 mph | 220 kmh
Empty Weight: 285 kg | 628 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 1:12
Take-off distance (50ft obstacle): 820 ft | 250 m
Landing distance (50ft obstacle): 720 ft | 220 m

Aircraft information:
Modern two seat microlight aircraft that are unique for its very good aerodynamics, excellent flight qualities and a high economy of operation.

Carefully designed shape of the fuselage that is made of glassfibre laminate and its high quality surface provide minimum air resistance and minimum sensibility to side wind. The wing as well as the tail plane are of metal construction covered in part with fabrics. The centre section of the wing is welded from steel tubes.

Aircraft have a uniquely spacious cabin, which guarantees comfort namely in long cross-country flights.

The position of the control stick between the seats makes getting in and out very comfortable. Large surface organic glass cover of the cabin offers a very good view.

Text from http://www.fantasyair.com/produkty/techinfo_en.html

Allegro 2000
Price: Not given

Fisher Flying Products
Super Koala


Stall: 28 kt | 32 mph | 51 kmh
Cruise: 61 kt | 70 mph | 113 kmh
VNE: 70 kt | 80 mph | 129 kmh
Empty Weight: 181 kg | 400 lbs
MTOW Weight: 376 kg | 830 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
Photo from: http://www.ultralightnews.com/ulbg2/fishersuperkoala.html

Super Koala
Price: Not given

Fisher Flying Products
Celebrity


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 74 kt | 85 mph | 137 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 272 kg | 600 lbs
MTOW Weight: 558 kg | 1230 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
The Celebrity is a biplane of wood construction with an optional steel fuselage, tandem seating (solo from the rear), fabric covered, light aircraft designed to be built in the experimental category. The Celebrity is designed for the first-time builder.

Landing & take-off not over 50ft obstacle.

Text and photo from: http://www.fisherflying.com

Celebrity
Price: 12650 USD

Fisher Flying Products
The Youngster


Stall: 28 kt | 32 mph | 51 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 181 kg | 400 lbs
MTOW Weight: 295 kg | 650 lbs
Climb Ratio: 700 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 250 ft | 76 m

Aircraft information:
This airplane offers you four-cycle dependability with the pleasure of flying a light, agile performer. The Youngster flies on the time proven 2315 airfoil with stainless wires and a bubble canopy. Enjoy the freedom of an open cockpit on warm summer days, and the warmth of a fully enclosed cockpit for comfortable flying in the winter.

Landing & take-off not over 50ft obstacle.

Text and photo from: http://www.fisherflying.com

The Youngster
Price: 8750 USD

Fisher Flying Products
R-80 Tiger Moth


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 254 kg | 560 lbs
MTOW Weight: 522 kg | 1150 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 400 ft | 122 m

Aircraft information:
Now you can relive a part of world history when you fly your own replica of the De Havilland Tiger Moth. You will sense the moments in history when thousands of British Commonwealth pilots were learning to fly in preparation for their part of World War II. With your leather helmet, goggles, gauntlets, and flying coat, you can relive some of the glory in aviation’s golden age. All of the excitement, charm, and nostalgia will be yours-except the expense of owning and maintaining the original De Havilland DH82 Tiger Moth.

Landing & take-off not over 50ft obstacle.

Text and photo from: http://www.fisherflying.com

R-80 Tiger Moth
Price: 15500 USD

Fisher Flying Products
Super Koala FP-202


Stall: 45 kt | 52 mph | 83 kmh
Cruise: 60 kt | 69 mph | 111 kmh
VNE: 95 kt | 109 mph | 176 kmh
Empty Weight: 201 kg | 443 lbs
MTOW Weight: 376 kg | 829 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 9:1
Take-off distance (50ft obstacle): 430 ft | 130 m
Landing distance (50ft obstacle): 560 ft | 172 m

Aircraft information:
FP-202 redefines the standard

With the Fisher FP 202 Koala, the standard for personal aircraft has been redefined, but not redesigned.

A strikingly faithful reproduction of one of the most popular aircraft ever built, the Koala can make the dream of owning a classic flying machine a reality.

Proven geodetic wood construction gives the FP202 its strength; proven Fisher ingenuity gives the plane its appeal. A totally enclosed cockpit provides plenty of room for the pilot, while economy of instrumentation and controls allow plenty of room for fun flying.

More classic-style aircraft hardware abounds: An aluminum strut braced main spar carrythrough, a ground adjustable horizontal stabilizer, 14-inch pneumatic tires with rubber shock cord, and removable cockpit panels for summer flight.

Text from: http://www.fisherflying.com/fleet/FP202/

Super Koala FP-202
Price: 14300 USD

Flight Design
CT2K


Stall: 33 kt | 39 mph | 62 kmh
Cruise: 127 kt | 146 mph | 235 kmh
VNE: 167 kt | 193 mph | 310 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 520 ft | 160 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Who doesn't dream of a sports aircraft that is comfortable, agile, has excellent visibility, a high cruise speed, and has a great range - while still having very reasonable acquisition and operating costs? An ultralight composite aircraft that is easily capable of flying more than 1,000 miles non-stop, such as from Germany to Italy, France, England or Spain?

With the Flight Design CT2K this dream becomes a reality! In close cooperation with our dealers and pilots, the CT has continued to develop and improve. Complying with the different regulations in different countries, the Flight Design CT2K has been developed, and now has less weight, increased power and higher performance, with additional load-carrying capability.

The ultraulight plane CT2K from Flight Design now has even greater application for flight training as well as for everyday operation. In addition, the Flight Design CT2K is now even more stable and easier to fly, while the quality of workmanship and reliability has reached a new standard of excellence.

The FlightDesign CT2K is built for the future. The design of the wing and the aircraft structure has been tested for a take-off weight up to 600 kg, so the Flight Design CT2K can comply with different certification criteria in different countries.

Visit: www.flightdesign.com

Photo: Tom J. www.pilots.nu

Text from: http://www.flightdesign.com/ultralight.html

CT2K
Price: 55862 EURO

Flight Design
CTSW ( also VLA )


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 130 kt | 149 mph | 240 kmh
VNE: 163 kt | 187 mph | 301 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 1:14
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 980 ft | 300 m

Aircraft information:
In spring 2003 CT2K has a new brother in CTSW. Due to 80 cm shorter wings and increased ground effect CTSW has even greater aerodynamic stability and is easy to land. This aircraft had 5 km/h increased maximum level-flight speed while having slightly reduced climb speed.

Both CT2K and CTSW is also available as VLA versions.

www.flightdesign.com

CTSW = CT Short Wing

Photo: Tom Johansson, http://www.tomotoaviation.com/

CTSW ( also VLA )
Price: 60000 EURO

Flightstar sportplanes
Spyder


Stall: 31 kt | 36 mph | 58 kmh
Cruise: 56 kt | 65 mph | 105 kmh
VNE: 83 kt | 96 mph | 154 kmh
Empty Weight: 127 kg | 280 lbs
MTOW Weight: 340 kg | 750 lbs
Climb Ratio: 660 ft/min | 3 m/s
Glide Ratio: 8:1
Take-off distance (50ft obstacle): 350 ft | 107 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
The Photo from http://www.flyflightstar.com/

Spyder
Price: Not given

Fly Synthesis
TEXAN RG


Stall: 33 kt | 39 mph | 62 kmh
Cruise: 127 kt | 146 mph | 235 kmh
VNE: 151 kt | 174 mph | 280 kmh
Empty Weight: 282 kg | 622 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1400 ft/min | 7,5 m/s
Glide Ratio: 15
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 460 ft | 140 m

Aircraft information:
Photo from: http://www.flysynthesis.com

TEXAN RG
Price: Not given

Fly Synthesis
TEXAN TOP CLASS


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 121 kt | 140 mph | 225 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 275 kg | 606 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: 14
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 460 ft | 140 m

Aircraft information:
The Texan is a two seat ultra-light plane. As a true three-axis low wing aircraft, it has been designed to get maximum performance when compared to the more traditional aircraft designs. With its high aerodynamic efficiency the Texan is a master at short take-off and landing runs, rapid climbs and fast cruises with modest fuel consumptions. A unique feature of the Texan design is the elevated level of flight comfort for the pilot and passenger alike. With excellent views, extra cabin space and the very low noise level inside the cockpit, occupants can now enjoy comforts usually found only in commercial aircraft.

Text and photo from: http://www.flysynthesis.com

TEXAN TOP CLASS
Price: Not given

Fly Synthesis
STORCH HS


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 116 kt | 134 mph | 215 kmh
Empty Weight: 246 kg | 542 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 14
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 390 ft | 120 m

Aircraft information:
Storch is an two seaters ultralight three-axis aircraft designed to get more elevated performances in comparison to the analogous traditional means. His tall aerodynamic efficiency allows short take-off and landing runs, rapid climbs and fast cruises with modest fuel consumptions.

Photo and text from: http://www.flysynthesis.com

STORCH HS
Price: Not given

Fly Synthesis
WALLABY


Stall: 27 kt | 31 mph | 50 kmh
Cruise: 62 kt | 71 mph | 115 kmh
VNE: 78 kt | 90 mph | 145 kmh
Empty Weight: 208 kg | 459 lbs
MTOW Weight: 425 kg | 937 lbs
Climb Ratio: 400 ft/min | 2,5 m/s
Glide Ratio: 9
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 300 ft | 90 m

Aircraft information:
Wallaby is an two seaters ultralight three-axis basic aircraft with open cockpit designed to get more elevated performances in comparison to the traditional basic ultralight aircraft. His simply configuration allows short take-off and landing runs and a good cruise speed with modest fuel consumptions. The philosophy of a basic aircraft cames with the security of composite materials and with the latest technologies.

Text and photo from: http://www.flysynthesis.com

WALLABY
Price: Not given

Flying Machines s.r.o.
B612


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 170 kg | 375 lbs
MTOW Weight: 300 kg | 661 lbs
Climb Ratio: 800 ft/min | 4,5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
For more information see Flying Machines at http://www.flyingmachines.cz

B612
Price: Not given

Flying Machines s.r.o.
Carbone one


Stall: 33 kt | 38 mph | 61 kmh
Cruise: 54 kt | 62 mph | 100 kmh
VNE: 81 kt | 93 mph | 150 kmh
Empty Weight: 209 kg | 461 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 0 ft/min | - m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Carbone one is all composite trike - new generation of modern powered hang glider. Light and strong structure, resistant, big bagage compartment, internal balistic parachute system,60l fuel tank.Promoted by Aviatec sarl.

Carbone one
Price: 24950 EURO

Flying Machines s.r.o.
FM250 Vampire


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 103 kt | 118 mph | 190 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 250 kg | 551 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: 15,4
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
New Two seat all composite, high performance ultralight ....designed to fit inside european ultralights regulations...empty weight 250kg ...

FM250 Vampire
Price: Not given

FLYLAB srl
Tucano Delta3 VTW


Stall: 30 kt | 34 mph | 55 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 92 kt | 106 mph | 170 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 0 kg | 0 lbs
Climb Ratio: 1600 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 200 ft | 60 m
Landing distance (50ft obstacle): 300 ft | 90 m

Aircraft information:
Twin Engine Ultralight! Puller and pusher engine!

Text and Photo: http://www.flylab.it/

The Tucano Delta3 VTW is directly derived from the twin-engined Tucano Delta3 TW, to which the same concepts that have led to the Tucano V have been coupled: cleaner aerodynamics, new cabin, new mudguards. The result is a machine with amazing performances for a true ultralight aircraft!

Tucano Delta3 VTW
Price: Not given

FLYLAB srl
Tucano


Stall: 28 kt | 32 mph | 52 kmh
Cruise: 54 kt | 62 mph | 100 kmh
VNE: 81 kt | 93 mph | 150 kmh
Empty Weight: 220 kg | 485 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 800 ft/min | 4,5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 230 ft | 70 m
Landing distance (50ft obstacle): 230 ft | 70 m

Aircraft information:
The Tucano is for sure the most sold and flown ultralight aircraft in Italy. Strong and reliable, it is suitable for beginners as much as for expert pilots, being also the most used ultralight in flight schools.

Text and Photo from: http://www.flylab.it

Tucano
Price: Not given

Fläming Air GmbH Oehna
Smaragd


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 119 kt | 137 mph | 220 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 290 kg | 639 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1200 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:
Unser Smaragd ist ein aus glas- und kohlefaserverstärktem Kunststoff gebauter konventioneller Tiefdecker mit klassischem Leitwerk und Dreibeinfahrwerk. Die Sitze sind nebeneinander angeordnet und verstellbar. Hinter den Sitzen befindet sich der sehr geräumige Gepäckraum und das Rettungsgerät. Die Flügelverankerung wird über ineinandergreifende Holmwurzeln und einen Hauptbolzen wie bei modernen Seglern gelöst, was eine extrem einfache Demontage erlaubt. Das Hauptfahrwerk besteht aus einer Gfk- Kevlar - Schwinge mit hydraulisch gebremsten Rädern. Die Tanks sind in den Flächen angeordnet. 60 bzw. 120 Liter stehen zur Verfügung.

Text and Photo from: http://www.flaemingair.de/

Smaragd
Price: Not given

Gimi Poland
kermitt 1


Stall: 0 kt | 0 mph | 0 kmh
Cruise: 0 kt | 0 mph | 0 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 33 kg | 73 lbs
MTOW Weight: 160 kg | 353 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:
Our paratrikes are completly shel composite (forcet with fibre glas) contruction witch gives them very light weight. One seat trike: lenght: 195 cm widh: 140 cm fuel tank (standard): 10 l. (placed inside trke under engine) Very strong construction, durable for hard landings, stainless steel basket, dissasembleable, protecting propeller from damage. composite landing gear, wheels 260 mm with bearing, automatic wing positioning system (simple contruction. Big trunk under the seat. www.gimilot.prv.pl e-mail gimilot@poczta.onet.pl

kermitt 1
Price: Not given

Gimi Poland
kermitt 2


Stall: 0 kt | 0 mph | 0 kmh
Cruise: 0 kt | 0 mph | 0 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 56 kg | 123 lbs
MTOW Weight: 270 kg | 595 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:
Our paratrikes are completly shel composite (forcet with fibre glas) contruction witch gives them very light weight. Fuel tank (standard): 10 l. (placed inside trke under engine). Very strong construction, durable for hard landings, stainless steel basket, dissasembleable, protecting propeller from damage. Composite landing gear, wheels 300 mm with bearing, automatic wing positioning system (simple contruction). Two seat trike: weight: 27 kg (without engine) lenght: 245 cm widh: 165 cm Ideal for training. www.gimilot.prv.pl e-mail gimilot@poczta.onet.pl

kermitt 2
Price: Not given

Golden Circle Air, Inc
T-Bird II (Akka - Tierra)


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 61 kt | 70 mph | 113 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 259 kg | 572 lbs
MTOW Weight: 544 kg | 1200 lbs
Climb Ratio: 1300 ft/min | 7 m/s
Glide Ratio: 7-1
Take-off distance (50ft obstacle): 350 ft | 107 m
Landing distance (50ft obstacle): 350 ft | 107 m

Aircraft information:
Introducing the T-Bird Line of kit aircraft. This plane is the most respected kit in the industry, and for good reason. It is absolutely the strongest and the easiest ultralight to build. The evolution of the T-Bird began in 1974. It is the oldest continually built ultralight ever.

Rough field operation, tail dragger or tri-gear, highwing pusher. Tube and fabric. 100 hour build. pre-sewn colored fabric. +6 -4 stress. able to leap tall building.

Text and photo from: http://www.goldencircleair.com/tbird_frame.htm

T-Bird II (Akka - Tierra)
Price: 18320 USD

Golden Circle Air, Inc
T-Bird I (Akka - Tierra)


Stall: 28 kt | 32 mph | 51 kmh
Cruise: 52 kt | 60 mph | 97 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 122 kg | 270 lbs
MTOW Weight: 272 kg | 600 lbs
Climb Ratio: 750 ft/min | 4 m/s
Glide Ratio: 7-1
Take-off distance (50ft obstacle): 160 ft | 49 m
Landing distance (50ft obstacle): 150 ft | 46 m

Aircraft information:
Introducing the T-Bird Line of kit aircraft. This plane is the most respected kit in the industry, and for good reason. It is absolutely the strongest and the easiest ultralight to build. The evolution of the T-Bird began in 1974. It is the oldest continually built ultralight ever.

Rough field operation, tail dragger or tri-gear, highwing pusher. Tube and fabric. 100 hour build. pre-sewn colored fabric. +6 -4 stress. able to leap tall building.

Text and photo from: http://www.goldencircleair.com/tbird_frame.htm

T-Bird I (Akka - Tierra)
Price: 12410 USD

Grupo Aeromot
Super Ximango AMT-200


Stall: 42 kt | 48 mph | 78 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 132 kt | 152 mph | 245 kmh
Empty Weight: 620 kg | 1367 lbs
MTOW Weight: 850 kg | 1874 lbs
Climb Ratio: 550 ft/min | 3 m/s
Glide Ratio: 31:1
Take-off distance (50ft obstacle): 1060 ft | 323 m
Landing distance (50ft obstacle): 950 ft | 290 m

Aircraft information:
Along the years, AEROMOT Aeronaves has become direct factory distributor for most of the leading manufacturers of the world in the areas of aircraft and their engines, instruments, avionics and other systems, including: EMBRAER/Neiva, Chincul, Textron Lycoming, TCM Ignition, Champion, Unison, Garmin, Trimble, Allied Signal Bendix/King, Collins, Ametek, Smiths, AIM, Cherry Textron, Edo-Aire, Pem Fasteners, Kollsman, etc. Text and photo from: http://www.ximango.com.br/ingles/

Super Ximango  AMT-200
Price: Not given

Gryf Aircraft
MD3 Rider


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 119 kt | 137 mph | 220 kmh
VNE: 148 kt | 171 mph | 275 kmh
Empty Weight: 275 kg | 606 lbs
MTOW Weight: 480 kg | 1058 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 phot from: http://gryfair.cz/aircraft/ Classical all-metal high-wing with side-by-side seats designed to be ideal for training, CROSS-COUNTRY flying and flying for fun.

MD3 Rider
Price: Not given

Gyrocopter
MT03 Turbo


Stall: 0 kt | 0 mph | 0 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 89 kt | 103 mph | 165 kmh
Empty Weight: 204 kg | 450 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1800 ft/min | 9 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 160 ft | 50 m
Landing distance (50ft obstacle): 30 ft | 10 m

Aircraft information:
Photo and info about Gyrokopter from plhttp://www.gyro-copter.de/

MT03 Turbo
Price: Not given

Homebuilt Aviation Pty Ltd
Cyclone


Stall: 44 kt | 51 mph | 81 kmh
Cruise: 115 kt | 132 mph | 213 kmh
VNE: 154 kt | 177 mph | 285 kmh
Empty Weight: 300 kg | 661 lbs
MTOW Weight: 544 kg | 1199 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
The Cyclone is designed around what pilots want in an aircraft. Including Geared EFI RG TT 2000 engine which leaps this aircraft into 2005 technology. Twin piston disc brakes, 6 inch wheels, 44 inch wide cockpit for comfort, bubble canopy for style, ribs and formers made and welded chrome molly components make assembly a lot quicker. Weight and balance worked out on more effective cruising requirements. Flys like a light plane. Package deals from $10,500 USD

Cyclone
Price: 30 USD

Homebuilt Aviation Pty Ltd
Typhoon


Stall: 38 kt | 44 mph | 70 kmh
Cruise: 95 kt | 109 mph | 176 kmh
VNE: 130 kt | 150 mph | 241 kmh
Empty Weight: 300 kg | 661 lbs
MTOW Weight: 544 kg | 1199 lbs
Climb Ratio: 1100 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 250 ft | 76 m
Landing distance (50ft obstacle): 400 ft | 122 m

Aircraft information:
The Typhoon designed around the 90 to 100 knot capability, nice wide 44 inch cockpit, dual piston disc brakes on 6 inch wheels required to hold the torque of the engine. Having most of the components or material supplied takes the guess work and time means more time to build. Metal has an inbuilt design strength,no glues NO SANDING, just straight out building. A well proportioned aircraft, a delight to fly available as Tri or Tail Dragger. Ideal for wet grass and beach landings to get you into those hard to get fishing spots with an engine that really has the grunt.

Typhoon
Price: 30000 USD

Humbert Aviation
Tetras


Stall: 30 kt | 34 mph | 55 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 113 kt | 130 mph | 210 kmh
Empty Weight: 284 kg | 626 lbs
MTOW Weight: 495 kg | 1091 lbs
Climb Ratio: 1300 ft/min | 7 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
The Photo from: http://www.humbert-aviation.com/album_en.htm

Tetras
Price: Not given

Humbert Aviation
The Moto Du Ciel (M.D.C.) 582


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 67 kt | 78 mph | 125 kmh
VNE: 81 kt | 93 mph | 150 kmh
Empty Weight: 173 kg | 381 lbs
MTOW Weight: 425 kg | 937 lbs
Climb Ratio: 1150 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
Photo from: http://www.humbert-aviation.com/album_en.htm

The Moto Du Ciel (M.D.C.) 582
Price: Not given

Hummel Aviation
UltraCrusier


Stall: 22 kt | 25 mph | 40 kmh
Cruise: 70 kt | 80 mph | 129 kmh
VNE: 83 kt | 95 mph | 153 kmh
Empty Weight: 115 kg | 254 lbs
MTOW Weight: 227 kg | 500 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 250 ft | 76 m

Aircraft information:
The UltraCruiser is a legal all metal ultralight with economical, reliable, four stroke power and cruise of 60 mph

Canopy and heater for year round flying, canopy can be removed quickly

Detachable wings for easy storage

Very docile, easy to fly

Excellent performance with 37 hp engine

Full size parts shown on plans

Very comfortable for long flights

Wide 6.5 ft. landing gear track for improved ground handling

Text and photo from: www.flyhummel.com

UltraCrusier
Price: Not given

I.C.P
Savannah


Stall: 24 kt | 28 mph | 45 kmh
Cruise: 76 kt | 87 mph | 140 kmh
VNE: 86 kt | 99 mph | 160 kmh
Empty Weight: 272 kg | 600 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 12:1
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 440 ft | 135 m

Aircraft information:
The Savannah is an ultralight STOL aircraft (short takeoff and landing) with two side-by-side seats, single high wing, tricycle landing gear and full metal (alluminium) construction.

It shares the same structure of the BINGO!, differing just in some minor details, the engines mounted and the equipment.

Photo From: http://www.icp-avio.com/index.htm

Savannah
Price: Not given

Ibis
GS240


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 104 kt | 120 mph | 193 kmh
VNE: 122 kt | 140 mph | 225 kmh
Empty Weight: 341 kg | 752 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 700 ft/min | 4 m/s
Glide Ratio: 14:1
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
The IBIS GS240 is an all-metal, high-wing aircraft manufactured by the IBIS Aircraft company in Colombia. The GS240 has specifications and performance that are within the limitations of the new Light Sport Aircraft category. The GS240 is available for the U.S. market as a "quick-build kit" that will still meet the requirements of the FAA "51% rule" and allow the GS 240 to be put into the Experimental (Amateur-Built) Category. The GS240 kit is intended to provide as short a building time as reasonably possible for the builder, with all difficult aspects of fabrication and assembly having been done at the factory to minimize complications and delay for the first-time builder.

The IBIS GS-240 has specifications and performance that allow it to fit within the new "Light Sport Aircraft" rules. With the GS240 in this category, it can be flown by existing Private and Recreational pilots (without them having to maintain an FAA Medical Certificate), but also by people holding the new "Sport Pilot" license.

For info about the new "Sport Pilot / Light Sport Aircraft" rules, visit the EAA www.sportpilot.org web site.

Text and Photo from: http://www.rlsa.us/ibis.htm

GS240
Price: Not given

Icarus Foundation
F99 Rambo


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 124 kt | 143 mph | 230 kmh
Empty Weight: 285 kg | 628 lbs
MTOW Weight: 475 kg | 1047 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 13
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 820 ft | 250 m

Aircraft information:
Aluminum construction, steel tube cabin, 118 cm wide.

electric elevator trim

carburator deicing

cabin vent as standard

contact: airsport99@hotmail.com

F99 Rambo
Price: 33000 EURO

Impulse Aircraft
Impulse 100 td


Stall: 33 kt | 39 mph | 62 kmh
Cruise: 130 kt | 149 mph | 240 kmh
VNE: 178 kt | 205 mph | 330 kmh
Empty Weight: 280 kg | 617 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1600 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 520 ft | 160 m
Landing distance (50ft obstacle): 850 ft | 260 m

Aircraft information:
The Impulse aircraft has a very sleek design and excellent performance. This aircraft is for all aviators!

Impulse 100 td
Price: Not given

Indus Aviation
Thorp T - 211


Stall: 39 kt | 45 mph | 72 kmh
Cruise: 107 kt | 123 mph | 198 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 352 kg | 775 lbs
MTOW Weight: 576 kg | 1270 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 450 ft | 137 m
Landing distance (50ft obstacle): 495 ft | 151 m

Aircraft information:
The Thorp T-211,was designed by the legendary aircraft designer, John Thorp. The original airplane was designed and type certificated in 1946 as the Thorp T11. Updated to 100 HP in the 1960’s, and designated the T211, it was completely re-engineered, modernized and re-certified by the FAA in 1990. Thorp Aero of Sturgis, Kentucky in 1990-91, manufactured the T 211 under an FAA Production Certificate. The project was stopped due to the economic climate of the times. IndUS Aviation acquired the rights to production, tooling and a large inventory of parts and spares, which launched our manufacture of this airplane.
----------------------
Editors note: take-off and landing distance not over 50ft obstacle

Text and photo from: http://www.indusav.com

Thorp T - 211
Price: Not given

INTERAVIA DESIGN BUREAU, MOSCOW
I-1L


Stall: 0 kt | 0 mph | 0 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 840 kg | 1852 lbs
Climb Ratio: 0 ft/min | - m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 920 ft | 280 m
Landing distance (50ft obstacle): 720 ft | 220 m

Aircraft information:
Aircraft Information from: http://www.ctrl-c.liu.se/misc/ram/i-1l.html

I-1L
Price: Not given

Interplane S.R.O
S2 Falcon


Stall: 33 kt | 38 mph | 61 kmh
Cruise: 118 kt | 136 mph | 219 kmh
VNE: 133 kt | 153 mph | 246 kmh
Empty Weight: 318 kg | 700 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 640 ft | 195 m
Landing distance (50ft obstacle): 600 ft | 183 m

Aircraft information:
Text and photo from http://www.interplaneusa.com/ This plane is also known as Qualt 201 or Flamingo

S2 Falcon
Price: Not given

Interplane S.R.O
S3 Eagle


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 104 kt | 120 mph | 193 kmh
VNE: 111 kt | 128 mph | 206 kmh
Empty Weight: 318 kg | 700 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1100 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 600 ft | 183 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
Text and photo from: http://www.interplaneusa.com/

S3 Eagle
Price: Not given

Interplane S.R.O
S1 Cobra


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 83 kt | 95 mph | 153 kmh
VNE: 111 kt | 128 mph | 206 kmh
Empty Weight: 318 kg | 700 lbs
MTOW Weight: 559 kg | 1232 lbs
Climb Ratio: 1050 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 101 m
Landing distance (50ft obstacle): 380 ft | 116 m

Aircraft information:
The S1 Cobra is formerly known as "The Skyboy" Text and photo from: http://www.interplaneusa.com/

S1 Cobra
Price: Not given

Ison Aircraft
Airbike


Stall: 23 kt | 26 mph | 42 kmh
Cruise: 56 kt | 65 mph | 105 kmh
VNE: 78 kt | 90 mph | 145 kmh
Empty Weight: 136 kg | 300 lbs
MTOW Weight: 254 kg | 560 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:
Text and photo from: http://www.ultralightflyer.com/airbike/ The Airbike has been in production since 1995. It mates a welded steel fuselage to an all wood wing.Standard features include an open cockpit, removable wings, steerable tailwheel, 4 point safety harness, fuel tank, factory welded fuselage and tail. Options include various engines, folding wings brakes, trim, wheel pants, wing tips bucket seat, extra fuel, plus various quick build and assembly packages. For more information contact ISON Aircraft • 10790 Ivy Bluff Road • Bradyville, TN 37026 Phone (615) 765-5397 • Fax (615) 765-7234 e-mail: isonair@dtccom.net

Airbike
Price: Not given

Italian Industrial initiatives S.P.A.
SkyArrow 450 TS


Stall: 33 kt | 38 mph | 61 kmh
Cruise: 97 kt | 112 mph | 180 kmh
VNE: 121 kt | 139 mph | 224 kmh
Empty Weight: 286 kg | 631 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1250 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 525 ft | 160 m
Landing distance (50ft obstacle): 558 ft | 170 m

Aircraft information:
The Sky Arrow UL/AUL is easy to fly, with superb visibility and low operating costs. The Sky Arrow UL/AUL is an out-standing personal aircraft, as well as an excellent trainer. Manufactured with corrosion-free carbon fibre sandwich, the airframe is extremely strong yet lightweight, resulting in an aircraft with exceptional take-off and flight performance.

Headroom, and dual side stick controls provide the ultimate in comfort and visibility for both pilot and passenger. Enjoy the spacious instrument panel, electric flap and elevator trim, low cockpit noise levels and baggage space for local flights or extended trips.

The Skyarrow is also available as a 480 kg version (480 TS).

Text and photo from: http://www.skyarrow.com/

SkyArrow 450 TS
Price: Not given

Jabiru Aircraft Pty
ST3 UL ( Calypso )


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 85 kt | 98 mph | 157 kmh
VNE: 116 kt | 133 mph | 215 kmh
Empty Weight: 253 kg | 558 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 1:14
Take-off distance (50ft obstacle): 1180 ft | 360 m
Landing distance (50ft obstacle): 1180 ft | 360 m

Aircraft information:
The New Jabiru Calypso has larger tail fin and elevator than the older Jabiru UL ST3. It has also winglets and higher cruise speed, about 95-100 knots.

ST3 UL ( Calypso )
Price: Not given

Jodel
D120


Stall: 28 kt | 32 mph | 52 kmh
Cruise: 95 kt | 109 mph | 176 kmh
VNE: 138 kt | 159 mph | 256 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 650 kg | 1433 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Jodel, a classic aircraft.

D120
Price: Not given

Jodel
D18 UL


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 94 kt | 109 mph | 175 kmh
VNE: 134 kt | 154 mph | 248 kmh
Empty Weight: 235 kg | 518 lbs
MTOW Weight: 460 kg | 1014 lbs
Climb Ratio: 700 ft/min | 3.5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 820 ft | 250 m
Landing distance (50ft obstacle): 1450 ft | 443 m

Aircraft information:
The photo from http://www.piteraq.dk/flight/jodel.html

D18 UL
Price: Not given

Johnston Aviation
Tiger Cub UL


Stall: 20 kt | 23 mph | 37 kmh
Cruise: 48 kt | 55 mph | 89 kmh
VNE: 78 kt | 90 mph | 145 kmh
Empty Weight: 136 kg | 300 lbs
MTOW Weight: 295 kg | 650 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: 8:1
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
Text and photo from: http://www.nb.net/~tigercub/

Tiger Cub UL
Price: Not given

JORA spol s.r.o.
JORA


Stall: 24 kt | 28 mph | 45 kmh
Cruise: 76 kt | 87 mph | 140 kmh
VNE: 87 kt | 101 mph | 162 kmh
Empty Weight: 225 kg | 496 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 500 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 260 ft | 80 m
Landing distance (50ft obstacle): 230 ft | 70 m

Aircraft information:
JORA aircraft is a two seat ultra light Airplane, with upper placed wings and front engine, two seats side by Side, and tail surface type T. Undercarriage is boward, has three wheels, the wheels of the main undercarriage are braked, bow wheel is operated, resilience is executed by indio-rubber blocks.

Construction of the airplane is a combination of laminate and wood, facing is made from polyester fabric. Centroplane is made from duralumin bugles, undercarriage is concocted from steel bugles.

Photo and text from: http://www.jora.cz

JORA
Price: Not given

Just Aircraft LLC
Escapade / Highlander


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 80 kt | 92 mph | 148 kmh
VNE: 115 kt | 132 mph | 213 kmh
Empty Weight: 240 kg | 529 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 880 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 1000 ft | 305 m
Landing distance (50ft obstacle): 1200 ft | 366 m

Aircraft information:
Two place side-by-side dual control sticks.

High quality 4130 Chrome moly steel.

Wings fold in under 2 minutes. No disconnecting of controls or surfaces.

Tail-wheel or tricycle landing gear, easy swap.

UK section S static and flight certification testing requirements.

Introduced at Arlington and Oshkosh 2004, HIGHLANDER is an upgraded version of the ESCAPADE. Just Aircraft's new bush plane qualifications are enhanced by a larger balanced elevator and rudder, a larger trim tab, extended (and beefed up) gear legs with larger wheels and brakes, gull wing doors (can be opened in flight), an 8" tail wheel and VG's. And, a new three foot longer wing! There's plenty of room too, 5'4" Rachelle can easily curl up for a nap in the cargo area!

Text and photo from: www.slowflight.com

Escapade / Highlander
Price: Not given

Kappa 77
KP 2U SOVA


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 143 kt | 165 mph | 265 kmh
Empty Weight: 285 kg | 628 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:
Retractable gear. The photo is from http://www.kappa77.cz/

KP 2U SOVA
Price: Not given

Kiebitzflieger
Kiebitz


Stall: 30 kt | 34 mph | 55 kmh
Cruise: 67 kt | 78 mph | 125 kmh
VNE: 76 kt | 87 mph | 140 kmh
Empty Weight: 220 kg | 485 lbs
MTOW Weight: 400 kg | 882 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:
Text and photo from: http://www.kiebitzflieger.de/index.htm

Kiebitz
Price: Not given

KLN
VL-3


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 119 kt | 137 mph | 220 kmh
VNE: 162 kt | 186 mph | 300 kmh
Empty Weight: 275 kg | 606 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1200 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:
The VL-3 is an ultralight, single-engine, low-wing aeroplane of classical design with a bow-type retractable or fixed landing-gear and two side-by-side seats. The plane has been certified according to regulation UL-2 of the Amateur Aeronautical Association of the Czech Republic for maximum take-off weight (MTOW) of 450 kg.

Harmonious aerodynamic shape and excellent flying performance make the aeroplane suitable for touring or recreational flying.

The VL 3 is being certified in UL catagory for MTOW 450 kg and for MTOW 560 kg according JAR - VLA.

The KLN VL3 airplane is manufactured by Karel Klenor - KLN, Choceň, the firm which is one of the biggest producers of omposites in the Czech Republic.

Text from http://www.kln.cz

VL-3
Price: Not given

kolbe u. states america
kolbe mk2


Stall: 27 kt | 31 mph | 50 kmh
Cruise: 70 kt | 81 mph | 130 kmh
VNE: 92 kt | 106 mph | 170 kmh
Empty Weight: 200 kg | 441 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 5 ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 160 ft | 50 m
Landing distance (50ft obstacle): 130 ft | 40 m

Aircraft information:
as more balistic paraschute the plane is on italy (CENTRE) for query info@aeromarinaservice.com call sergio italy +39 337/318349

kolbe mk2
Price: 9000 EURO

Lambert Aircraft Engineering
Mission M106


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 114 kt | 132 mph | 212 kmh
Empty Weight: 260 kg | 573 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 9
Take-off distance (50ft obstacle): 920 ft | 280 m
Landing distance (50ft obstacle): 980 ft | 300 m

Aircraft information:
The Mission M106 is now available as a factory built Microlight (ULM/UL) category aircraft with tailwheel or nosewheel. It is standard fitted with a state of the art UL260i engine and glass cockpit. For more info: www.lambert-aircraft.com

Mission M106
Price: 36900 EURO

Leza Air Cam
Drifter XP-503


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 52 kt | 60 mph | 97 kmh
VNE: 74 kt | 85 mph | 137 kmh
Empty Weight: 175 kg | 385 lbs
MTOW Weight: 356 kg | 785 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:
A T.U.F. VIEW The Drifter series of aircraft were first introduced in early 1984 and were one of the most durable aircraft designs of its time. So much so that Lockwood Aviation has reintroduced the design. The wire braced craft has the front pilot sitting out in front of the wing on a tube surrounded by a small pilot pod and windscreen.

When powered by the 582 Rotax engine the craft will climb out at 900 feet a minute cruise a 70 m.p.h. and stall in the 38/40 m.p.h. range. Great little aeroplane for sight seeing or photography, a little too open for most winter conditions in Canada.

Photo and Text From: http://www.ultralightnews.com/ulbg2/lockwood.html

Drifter XP-503
Price: Not given

Leza Air Cam
Air-Cam


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 472 kg | 1040 lbs
MTOW Weight: 762 kg | 1680 lbs
Climb Ratio: 1500 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 200 ft | 61 m

Aircraft information:
Air-Cam, Twin engine light aircraft

Air-Cam
Price: Not given

Luscombe
8A


Stall: 37 kt | 43 mph | 69 kmh
Cruise: 91 kt | 105 mph | 169 kmh
VNE: 122 kt | 140 mph | 225 kmh
Empty Weight: 340 kg | 750 lbs
MTOW Weight: 572 kg | 1260 lbs
Climb Ratio: 550 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 1950 ft | 594 m
Landing distance (50ft obstacle): 1540 ft | 469 m

Aircraft information:
Luscombe Models 8A, 8B, and 8C meet the criteria for a Light Sport Aircraft.

8A
Price: 15000 USD

Mainair
Mercury


Stall: 22 kt | 25 mph | 41 kmh
Cruise: 45 kt | 52 mph | 83 kmh
VNE: 89 kt | 102 mph | 165 kmh
Empty Weight: 150 kg | 331 lbs
MTOW Weight: 370 kg | 816 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 1:8
Take-off distance (50ft obstacle): 600 ft | 184 m
Landing distance (50ft obstacle): 750 ft | 230 m

Aircraft information:
Mainair Mercury

Mainair Sports are the longest established manufacturer of microlight aircraft in Great Britain, and has been producing top quality aircraft since 1982 when microlight aircraft first began as a sport in the UK.

Since the early beginnings Mainair Sports have been at the forefront of weight-shift microlight design. They were the first company to be granted the prestigious Civil Aviation Authority (CAA) Company Approval for manufacturing of microlight aircraft and one of the first to have their aircraft approved by the CAA, against the exacting standards of British Civil Airworthiness Requirements Section S.

Mainair Sports operate from a modern industrial unit located in Rochdale near Manchester, Great Britain.

Text from: http://www.pmaviation.co.uk/

Mercury
Price: 12000 EURO

Martin Wezel Flugzeugtechnik
Apis 2


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 204 kg | 450 lbs
MTOW Weight: 300 kg | 661 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 39:1
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Text and photo from www.apis2.com

Apis 2 ...taste the freedom

Discovering the love for soaring is usually generating a love for a lifetime. And it is about the same with discovering the simplicity Ultralight flying offers. Creating a symbiosis of the two was therefore a logical and meaningful approach.

Easy and independent take off – like an Ultralight aircraft and still flies like a modern glider. That is the Apis 2.

Apis 2
Price: Not given

Micro Aviation
Bantam


Stall: 23 kt | 26 mph | 43 kmh
Cruise: 56 kt | 64 mph | 104 kmh
VNE: 80 kt | 92 mph | 148 kmh
Empty Weight: 176 kg | 388 lbs
MTOW Weight: 430 kg | 948 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 7:1
Take-off distance (50ft obstacle): 100 ft | 30 m
Landing distance (50ft obstacle): 100 ft | 30 m

Aircraft information:
The Bantam B22 was entirely developed in New Zealand by Max Clear, the owner of Micro Aviation

Ltd. The factory is located in the idyllic dairy farming country at Te Kowhai in the North Island and has been turning out Bantam aircraft in one form of another since 1983.

Designed around the proven American Phantom ultralight, the original Bantam, the B10 (so named because ten people worked on the project together) took to the air towards the end of 1983 and was a fairly basic single seat design powered by a Rotax 503 air-cooled engine.

Continuing development and improvements to the design resulted in the B20 model, still a single seat design but now boasting pull-on sailcloth and fully fabricated wing ribs. About 20 of these were made (some even finding their way over to Australia) but requests kept flooding in to the factory for a two-seater version and it was not long before the B22 came on the scene. Sporting dual seats and controls. And with a more powerful Rotax 582 engine, it became the standard production model in 1986.

Not that development stopped here either, although all of the above models were Type approved in New Zealand, it was found that in order to gain both International recognition and approval to use the aircraft as a trainer, called for the production of a fully Certified version.

As a result the factory geared itself up for this mammoth task. The wing was re-designed with a wider chord, shorter span and Clark-Y airfoil section. Changes were also made to the tail section, flaperons and cockpit, to name a few. The New Zealand Department of Civil Aviation supervised, tested and advised throughout this long drawn out process, finally awarding the new B22S fullCertification status in 1995 The Bantam B22S and B22J (with the new Jabiru 4-stroke engine) models are marketed in a number in a number of countries with in excess of 240 units having been produced. A paraplegic version with modified flght controls is also available.

Text and Photo from: http://www.microaviationsa.co.za/

Bantam
Price: Not given

MICROLEVE
ML-500


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 220 kg | 485 lbs
MTOW Weight: 500 kg | 1102 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 12:1
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 330 ft | 100 m

Aircraft information:
Basic ultralight, tricycle landing gear, with rigid wing. Now with a full closed cabin.

ML-500
Price: 14 USD

MICROLEVE
CORSARIO MK-5


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 90 kt | 104 mph | 167 kmh
VNE: 120 kt | 138 mph | 222 kmh
Empty Weight: 330 kg | 728 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 490 ft | 150 m

Aircraft information:
www.microleve.com.br microleve@microleve.com.br

CORSARIO MK-5
Price: 17000 USD

Minicab
GY 20


Stall: 38 kt | 43 mph | 70 kmh
Cruise: 97 kt | 112 mph | 180 kmh
VNE: 107 kt | 123 mph | 198 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 485 kg | 1069 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 1150 ft | 350 m
Landing distance (50ft obstacle): 1080 ft | 330 m

Aircraft information:
The Minicab was designed by Yves Gardan in 1949. Produced in limited numbers between 1952 and 1958. the design was acquired by A.W. Ord-Hume in Britain, who anglicised the plans. Adjusted them for home builders, the aircraft has subesequently proved extremely popular. The aircraft is marketed in North America as the Hawk BM.4 by Miranda Aircraft of Canada.

GY 20
Price: Not given

Murphy Aircraft MFG. LTD
Renegade


Stall: 31 kt | 36 mph | 58 kmh
Cruise: 70 kt | 80 mph | 129 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 181 kg | 400 lbs
MTOW Weight: 431 kg | 950 lbs
Climb Ratio: 700 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 500 ft | 152 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
The open cockpit biplane has a certain nostalgic eye appealing quality which is reflected in the Renegade and even more so in the Renegade Spirit. Pilots who have flown biplanes regard them highly for their outstanding performance and handling characteristics. Those same qualities have also been incorporated into the Murphy Renegade Line. Text from: http://www.murphyair.com/Product_Info/Renagade/Introduction.htm

Renegade
Price: Not given

Murphy Aircraft MFG. LTD
Maverick


Stall: 24 kt | 28 mph | 45 kmh
Cruise: 70 kt | 80 mph | 129 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 200 kg | 440 lbs
MTOW Weight: 431 kg | 950 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
Murphy Maverick A side by side seated, high wing airplane has always had great appeal to a wide variety of flyers. From the every day pilot who likes to fly around his own patch to the outdoorsman or others who want to land in small strips, many pilots prefer the Murphy Maverick for it’s performance, visibility and visual appeal. Text and photo from: http://www.murphyair.com/Product_Info/Mav/Introduction.htm

Maverick
Price: Not given

NGAero
prototype


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 146 kt | 168 mph | 270 kmh
VNE: 162 kt | 186 mph | 300 kmh
Empty Weight: 260 kg | 573 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 0 ft/min | - m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Aircraft in development. Please visit www.ngaero.com

prototype
Price: 60000 EURO

Nibbio S.r.l.
Ramphos


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 59 kt | 68 mph | 110 kmh
VNE: 78 kt | 90 mph | 145 kmh
Empty Weight: 210 kg | 463 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): 0 ft | 0 m

Aircraft information:
Emerging from its earthbound roots and growing wings to fly into the unbound, RAMPHOS is an amphibious flying hull with wings made of anti-UV mylar of 15 mq. mounted as standard. Wings up to 21mq or the new strong foldable wing (tested +6/-36)can be mounted too. Ramphos comes as three-cycle configuration, where different engine size can be mounted ranging from 50 to 80 Hp (Rotax, Hirt, etc.). The propeller can be both two or three bladed, made of wood or composite material. The propeller ring functions as a protective as well as an anti-noise device.

Photo and Text from: http://ramphos.com/

Ramphos
Price: Not given

Norman Aviation International Inc.
Mini-Explorer


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 113 kt | 130 mph | 209 kmh
Empty Weight: 297 kg | 654 lbs
MTOW Weight: 559 kg | 1232 lbs
Climb Ratio: 850 ft/min | 4 m/s
Glide Ratio: n/a
Take-off distance (50ft obstacle): 400 ft | 122 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
2 Seater side by side. Bed for 2 at the back. No flaps. Made of wood, tubing and fabric. Wheel, skis or floats.

Mini-Explorer
Price: 34500 USD

Norman Aviation International Inc.
Nordic 6


Stall: 33 kt | 38 mph | 61 kmh
Cruise: 100 kt | 115 mph | 185 kmh
VNE: 117 kt | 135 mph | 217 kmh
Empty Weight: 264 kg | 582 lbs
MTOW Weight: 559 kg | 1232 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: n/a
Take-off distance (50ft obstacle): 400 ft | 122 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
2 seater side-by-side. Made of wood, tubing and fabric. Wheels, floats and skis. Titanium landing gear.

Nordic 6
Price: 19895 USD

Norman Aviation International Inc.
J-6 Karatoo


Stall: 33 kt | 38 mph | 61 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 87 kt | 100 mph | 161 kmh
Empty Weight: 249 kg | 550 lbs
MTOW Weight: 476 kg | 1050 lbs
Climb Ratio: 500 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 350 ft | 107 m

Aircraft information:
Karatoo, J-6 Karatoo, Norman Aviation J-6 Karatoo

Text and Photo from: http://www.ultralightflyer.com/karatoo/

J-6 Karatoo
Price: Not given

OSKBES MAI
MAI-223


Stall: 38 kt | 44 mph | 71 kmh
Cruise: 97 kt | 112 mph | 180 kmh
VNE: 105 kt | 121 mph | 195 kmh
Empty Weight: 320 kg | 705 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 800 ft/min | 4.2 m/s
Glide Ratio: N/A
Take-off distance (50ft obstacle): 1180 ft | 360 m
Landing distance (50ft obstacle): 950 ft | 290 m

Aircraft information:
MAI-223 is a single-engine twoseater semicantilever monoplane-parasol with non-retractable landing gear. Perfect controllability in all channels and an excellent pilot view from the cockpit make the plane extremely safe and pleasant for piloting. High thrust-to-weight ratio, high-lift device and landing gear with tail wheel allow to use airplane from short, unprepared runways. Floats and ski landing gear are enabled. Due to the folding wing airplane is very convenient for storage and transportation.

MAI-223
Price: 27150 EURO

PARAFAN Poland
Engine Powered Parachute Wing PARAFAN


Stall: 0 kt | 0 mph | 0 kmh
Cruise: 24 kt | 28 mph | 45 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 100 kg | 220 lbs
MTOW Weight: 200 kg | 441 lbs
Climb Ratio: 400 ft/min | 2 m/s
Glide Ratio: 4
Take-off distance (50ft obstacle): 130 ft | 40 m
Landing distance (50ft obstacle): 100 ft | 30 m

Aircraft information:
One of the first engine powered parachute wing vehicle was designed in Poland in mid-eighties, by aeronautical engineers: Marek Debski Ph.D. and Andrzej Komor Ph.D. The communicate provides some information concerning that early project. The power unit consisted of the KFM piston engine and two counter-rotating over-ducted propellers. Such idea was selected in order to eliminate possible gyro effects and due to this, to facilitate vehicle’s handling. The power unit was mounted on a vehicle’s carriage. Wide stretched analytical investigated by use of a specially prepared ground test bed. All the structure ( i.e. the carriage and parachute) was easily demounted and packed into a car luggage compartment for transport purposes. Info & Contact: dedal@ilot.edu.pl

Engine Powered  Parachute Wing PARAFAN
Price: Not given

Pathmaker
JK-05


Stall: 30 kt | 34 mph | 55 kmh
Cruise: 96 kt | 110 mph | 177 kmh
VNE: 111 kt | 128 mph | 206 kmh
Empty Weight: 280 kg | 617 lbs
MTOW Weight: 560 kg | 1235 lbs
Climb Ratio: 1600 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 490 ft | 149 m
Landing distance (50ft obstacle): 390 ft | 119 m

Aircraft information:
Pathmaker JK-05 was designed by Polish world renowned aeronautical engineer named Jerzy Krawczyk. he teamed up with Henryk Slowik, a businessman who played a big role in many huge projects and together they created an airplane that many people fell in love with. Pathmaker doesn't only look good, it flies even better.

Its concept was put on a drawing board in 1992 . Jerry is known better among soaring fraternity by number of gliders that he designed. One of more successful ones was Puchatek. This design is flying in Canada, the United States, Australia, Europe and many other countries.

The Pathmaker JK-05 is a high-wing monoplane of composite construction based on vinylester resins reinforced by glass and carbon fibres.

The Pathmaker JK-05 requires very little maintenance due to a fact that all the control systems use torque tubes, and being composite built reduces regular maintenance to pre-flight inspection and cleaning.

Tex and photo from: http://www.skypaths.net/overview.htm

JK-05
Price: Not given

Pegasus
Quick


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 100 kt | 115 mph | 185 kmh
Empty Weight: 209 kg | 461 lbs
MTOW Weight: 409 kg | 902 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 680 ft | 206 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
The QUIK is at the cutting edge of flexwing development. Offering speed, climb performance, comfort, quietness and above all relaxed flying in weather conditions avoided by the normal flexwing pilot. It’s light handling small wing with “hands off” trim speed in excess of 80 mph, and a level speed of 100 mph makes distance touring a reality and ground handling simplicity itself. The Quantum’s 409 kg MAUW is retained, but the payload has increased due to the aircraft’s lighter weight. Finally, we listened to Quantum owners telling us how they would like the already superb comforts of the Quantum enhanced, this resulted in larger seating, more rearward headroom for the passenger and more wind protection.

Photo and Text from: http://www.pegasusaviation.co.uk/Quik.htm

Quick
Price: Not given

Petari-Boju Aviation Ltd.
Kit-Flight 3


Stall: 33 kt | 39 mph | 62 kmh
Cruise: 97 kt | 112 mph | 180 kmh
VNE: 113 kt | 130 mph | 210 kmh
Empty Weight: 290 kg | 639 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 350 ft/min | 2 m/s
Glide Ratio: 12
Take-off distance (50ft obstacle): 720 ft | 220 m
Landing distance (50ft obstacle): 920 ft | 280 m

Aircraft information:
price given on basic instrumentation, without avionic, BRS included also available as LSA/VLA

Kit-Flight 3
Price: 49000 EURO

Pietenpol
Air Camper


Stall: 40 kt | 46 mph | 74 kmh
Cruise: 70 kt | 81 mph | 130 kmh
VNE: 90 kt | 104 mph | 167 kmh
Empty Weight: 277 kg | 610 lbs
MTOW Weight: 451 kg | 995 lbs
Climb Ratio: 500 ft/min | 3 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 150 ft | 46 m
Landing distance (50ft obstacle): 250 ft | 76 m

Aircraft information:
The Pietenpol Air Camper continues to be a successful design for the same reasons homebuilders were so fascinated by the design 67 years ago. It still has graceful styling, predictable flying qualities, and easy construction.

Text and photo from: http://www.pressenter.com/~apietenp/

Note: Landing and take-off distance not over 50fr obstacle.

Air Camper
Price: Not given

Piper
J3 Cub


Stall: 33 kt | 38 mph | 61 kmh
Cruise: 65 kt | 75 mph | 120 kmh
VNE: 76 kt | 87 mph | 141 kmh
Empty Weight: 290 kg | 639 lbs
MTOW Weight: 500 kg | 1102 lbs
Climb Ratio: 450 ft/min | 2 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 730 ft | 223 m
Landing distance (50ft obstacle): 470 ft | 143 m

Aircraft information:
Piper J-3 Cub is maybe one of the most famous aircraft in our times. It is truley a workhorse!

ln 1938 Piper introduced the improved J-3 Cub. Powered by 40-hp Continental, Lycoming or Franklin engines, the J-3 sold for $1,3OO. Engine horsepower was soon raised to fifty and reached sixty-five by 194O. Piper also standardized a color scheme; just as Henry Fords Model T's were all black so Wiliiam Piper's Cubs were all bright yellow with black trim.

By 1947, when production ended, 14,125 Piper Cubs had been built. The J-3 is now finding an ever-increasing popularity among antique airplane buffs, and brand new Cubs are being constructed by homebuilders. Both an excellent trainer and a delightful sport plane, which lends itself to lazy summer afternoons, the Cub might best be summed up by the words simple, economical. and above all slow. The high demand for J3 Cubs is because of three basic facts: they are very nostalgic, they are lots of fun, they are cute as a bug. (But this has caused a high market demand which has driven the cost for a nice J3 out of sight for the average person).

Text from: http://www.geocities.com/CapeCanaveral/Lab/4515/cub.htm

J3 Cub
Price: Not given

Pipistrel d.o.o. Ajdovscina
Sinus 503


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 92 kt | 106 mph | 170 kmh
VNE: 121 kt | 140 mph | 225 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 600 ft/min | 3.2 m/s
Glide Ratio: 1:28
Take-off distance (50ft obstacle): 710 ft | 215 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
The PIPISTREL SINUS is the world's first ULM certified composite two seater motorglider.

You like sailing? Our vario propeller with in the air adjustable pitch and possibility to set it in the flag position transform your pipistrel Sinus in a real low resistance glider. All options are included in the basic price:

Electric starter, recycling fuel pump to fill the wing tanks, warning lights for fuel minimum level, cockpit hot air heating system, main wheel fairings, all engine and flight instruments, etc.

Please log on to www.pipistrel.si

Sinus 503
Price: 46900 EURO

Pipistrel d.o.o. Ajdovscina
Sinus 912


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 121 kt | 140 mph | 225 kmh
Empty Weight: 284 kg | 626 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1300 ft/min | 6.5 m/s
Glide Ratio: 1:27
Take-off distance (50ft obstacle): 500 ft | 153 m
Landing distance (50ft obstacle): 720 ft | 220 m

Aircraft information:
Pipistrel Sinus 912 was World Champion 2001/2002.

The PIPISTREL SINUS is the world's first ULM certified composite two seater motorglider.

You like sailing? Our vario propeller with in the air adjustable pitch and possibility to set it in the flag position transform your pipistrel Sinus in a real low resistance glider. All options are included in the basic price:

Electric starter, recycling fuel pump to fill the wing tanks, warning lights for fuel minimum level, cockpit hot air heating system, main wheel fairings, all engine and flight instruments, etc.

Please log on to www.pipistrel.si

Sinus 912
Price: 57900 EURO

Pipistrel d.o.o. Ajdovscina
Virus 912


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 121 kt | 140 mph | 225 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 284 kg | 626 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1200 ft/min | 6.2 m/s
Glide Ratio: 1:24
Take-off distance (50ft obstacle): 560 ft | 172 m
Landing distance (50ft obstacle): 720 ft | 220 m

Aircraft information:
Please log on to www.pipistrel.si

Virus 912
Price: 57900 EURO

Pipistrel d.o.o. Ajdovscina
Taurus 503


Stall: 33 kt | 39 mph | 62 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 121 kt | 140 mph | 225 kmh
Empty Weight: 279 kg | 615 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 800 ft/min | 3.9 m/s
Glide Ratio: 1:41
Take-off distance (50ft obstacle): 1080 ft | 330 m
Landing distance (50ft obstacle): 1080 ft | 330 m

Aircraft information:
Taurus is the world's first side-by-side microlight motorglider.

Please log on to www.pipistrel.si

Taurus 503
Price: 70000 EURO

Polaris srl
FIB - Flying Inflatable Boat


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 38 kt | 43 mph | 70 kmh
VNE: 43 kt | 50 mph | 80 kmh
Empty Weight: 216 kg | 476 lbs
MTOW Weight: 406 kg | 895 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 photo is from http://www.polarismotor.it/

FIB - Flying Inflatable Boat
Price: Not given

POLIMEX-CEKOP & PZL-KROSNO
DEKO-7


Stall: 40 kt | 47 mph | 75 kmh
Cruise: 103 kt | 118 mph | 190 kmh
VNE: 151 kt | 174 mph | 280 kmh
Empty Weight: 490 kg | 1080 lbs
MTOW Weight: 710 kg | 1565 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 12
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
DEKO-7: Very light training and observation aircraft (idea), was designed by Polish aeronautical engineers Marek Debski and Krzysztof Kotlinski. Type: Two-seat (side-by-side), single-engined, very light training and observation aircraft satisfying JAR-VLA requirements. Wing, fuselage and elevator are made of aluminum. Cockpit canopy is made of glass composite and plexiglas. Power Plant: One PZL Franklin 4A of 85 kW (116 hp), optionally Rotax or Jabiru Propeller: Junkers three-blade, carbon fiber, ground-adjustable pitch propeller. System: Ballistic parachute recovery system More info: http://www.dkd1970.webpark.pl/ Contact: dedal@ilot.edu.pl

DEKO-7
Price: Not given

Pro-Fe
Banjo


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 59 kt | 68 mph | 110 kmh
VNE: 73 kt | 84 mph | 135 kmh
Empty Weight: 157 kg | 346 lbs
MTOW Weight: 260 kg | 573 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 28:1
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
-

Banjo
Price: Not given

Progressive Aerodyne, INC
Searey


Stall: 36 kt | 42 mph | 68 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 100 kt | 115 mph | 185 kmh
Empty Weight: 372 kg | 820 lbs
MTOW Weight: 621 kg | 1370 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 350 ft | 107 m
Landing distance (50ft obstacle): 350 ft | 107 m

Aircraft information:
-

Searey
Price: Not given

Pulsar Aircraft Corporation
Super Pulsar 100


Stall: 48 kt | 55 mph | 89 kmh
Cruise: 181 kt | 208 mph | 335 kmh
VNE: 191 kt | 220 mph | 354 kmh
Empty Weight: 340 kg | 750 lbs
MTOW Weight: 635 kg | 1400 lbs
Climb Ratio: 2200 ft/min | 11 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 500 ft | 152 m
Landing distance (50ft obstacle): 800 ft | 244 m

Aircraft information:
Designed around the same beautiful lines as the legendary Pulsar XP, the Super Pulsar 100 was introduced by Pulsar Aircraft Corporation In August 2001. A high performance sport airplane capable of cruising at speeds over 200 mph but yet docile and safe for low time pilots . It\'s 2500 fpm climb will leave you breathless and it\'s docile and slow flight stability lets you land on short fields. 38 gallon fuel capacity for seven hours of endurance and 1250 mile range.

Super Pulsar 100
Price: Not given

Quad City Aircraft Corp.
Challenger II


Stall: 22 kt | 25 mph | 40 kmh
Cruise: 61 kt | 70 mph | 113 kmh
VNE: 74 kt | 85 mph | 137 kmh
Empty Weight: 141 kg | 310 lbs
MTOW Weight: 363 kg | 800 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 200 ft | 61 m

Aircraft information:
Challenger II

Photo from: http://www.quadcitychallenger.com/

Note: Take-off and Landing distance not over 50ft obstacle

Challenger II
Price: 16 USD

Quicksilver Mfg
GT 500


Stall: 36 kt | 42 mph | 68 kmh
Cruise: 72 kt | 83 mph | 134 kmh
VNE: 79 kt | 91 mph | 146 kmh
Empty Weight: 289 kg | 638 lbs
MTOW Weight: 499 kg | 1100 lbs
Climb Ratio: 655 ft/min | 3 m/s
Glide Ratio: 7:1
Take-off distance (50ft obstacle): 621 ft | 189 m
Landing distance (50ft obstacle): 905 ft | 276 m

Aircraft information:
The Quicksilver GT-500 development program was started with the goal of producing the best performing Quicksilver ever. Quicksilver’s aim was to design an aircraft that would change the category of ultralight & provide general aviation with the entry level aircraft it desperately needed. The focus was on more speed, better aerodynamics, and a greater range.

Photo and text from: http://www.quicksilveraircraft.com/gt500.htm

GT 500
Price: Not given

Quicksilver Mfg
MX II Sprint


Stall: 23 kt | 27 mph | 43 kmh
Cruise: 44 kt | 51 mph | 82 kmh
VNE: 65 kt | 75 mph | 121 kmh
Empty Weight: 147 kg | 325 lbs
MTOW Weight: 327 kg | 720 lbs
Climb Ratio: 595 ft/min | 3 m/s
Glide Ratio: 4.5:1
Take-off distance (50ft obstacle): 352 ft | 107 m
Landing distance (50ft obstacle): 240 ft | 73 m

Aircraft information:
The Quicksilver MXII SPRINT is ideal for the recreational flyer and flight schools. Its high lift partial double surfaced wings give it an exceptionally short take off roll and predictable handling at very low flight speeds. These characteristics make the Quicksilver MXII SPRINT easier to learn to fly than anything in its class. When equipped with floats, the Quicksilver MXII SPRINT's high lift wing will get you out of the water quicker and landing slower. Like all Quicksilvers, the MXII SPRINT's simple design and bolt together construction make preflight inspection and maintenance a breeze.

Photo and Text from http://www.quicksilveraircraft.com/

MX II Sprint
Price: Not given

Quicksilver Mfg
GT 400


Stall: 23 kt | 27 mph | 43 kmh
Cruise: 50 kt | 58 mph | 93 kmh
VNE: 53 kt | 61 mph | 98 kmh
Empty Weight: 125 kg | 276 lbs
MTOW Weight: 259 kg | 570 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 7:1
Take-off distance (50ft obstacle): 215 ft | 66 m
Landing distance (50ft obstacle): 350 ft | 107 m

Aircraft information:
The Quicksilver GT 400 Spring loaded steerable nose wheel

four position flaps

state-of-the-art landing gear suspension

virtually vibration-free engine mount

lowest cockpit noise level of all ultralights tested

58 mph cruise

tapered wing

short take-off and landing

airspeed indicator

quick set-up and breakdown

adjustable pilot seat

extraordinary visibility

delivered in easy-to-assemble-kit

optional 50 hp 503 Rotax engine.

Photo and Text from: http://www.quicksilveraircraft.com/gt400.htm

GT 400
Price: Not given

Quicksilver Mfg
Sport 2S


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 53 kt | 61 mph | 98 kmh
VNE: 76 kt | 87 mph | 140 kmh
Empty Weight: 195 kg | 430 lbs
MTOW Weight: 452 kg | 996 lbs
Climb Ratio: 500 ft/min | 3 m/s
Glide Ratio: 5.5:1
Take-off distance (50ft obstacle): 660 ft | 201 m
Landing distance (50ft obstacle): 484 ft | 148 m

Aircraft information:
The Quicksilver Sport 2S is the latest evolution in Quicksilver's open cockpit design.

The Quicksilver Sport 2S development program began with the goal of producing the best side-by-side trainer ever. Featuring strutted wings, wider cockpit, rugged aluminum steerable nosewheel, and larger wheels, the Quicksilver Sport 2S combines the many suggestions and comments of ultralight enthusiasts and professionals with Quicksilver's extensive designing, engineering, and R & D testing to fullfill that goal.

Pilots used to the docile and predictable flying qualities of the Quicksilver MX line of ultralight planes will be pleased with the Quicksilver Sport 2S. It provides the solid feel of a strut braced plane with the desirable flying characteristics that have made Quicksilvers so popular.

The Quicksilver Sport 2S' thoroughly engineered design and complete factory and dealer support help to make your flying as enjoyable as possible. Quicksilvers are the easiest kits on the market to assemble. An improved wing cover design makes the Sport 2S even faster to build. You are ready to fly with only a few weekends and some basic tools. Aircraft grade hardware and custom fittings allow for exceptional ease of assembly, maintenance, and breakdown for storage. In about thirty minutes you can go from trailer to flight. The Sport Quicksilver 2S boasts a wealth of new features.

Text and Photo from: http://www.quicksilveraircraft.com/SportIIS.html

Sport 2S
Price: Not given

Quicksilver Mfg
MX Sport


Stall: 23 kt | 27 mph | 43 kmh
Cruise: 46 kt | 53 mph | 85 kmh
VNE: 64 kt | 74 mph | 119 kmh
Empty Weight: 115 kg | 254 lbs
MTOW Weight: 238 kg | 525 lbs
Climb Ratio: 850 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 250 ft | 76 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
Quicksilver MX

For those of you who wanted more!

Created for the discriminating pilot who wants the excitement of a great performing airplane.

WE LISTEN TO YOU.

When we introduced the MX Sprint, it was greeted with resounding approval. But some people wanted even more performance. So, for those of you who wanted more, we now proudly introduce the MX Sport.

The MX Sport was designed to enhance the envelope of your flying pleasure. Its sleek, shortspan double-surface wing with full-span ailerons and conventional three-axis controls give the MX Sport a faster roll rate, greater speed range and better crosswind capability. Its 42 horsepower Rotax 447 engine and large 66-inch propeller give the Sport an exceptional climb rate.

The MX Sport comes standard with Quicksilver's world-renowned quality and a six-month written limited warranty. (See dealer for details.) We are the only manufacturer in the industry with enough confidence in our products to make such an offer.

All Quicksilver kits feature easy-to-assemble construction -- we do all the fabrication, you just bolt it together. Where other kits give you raw materials, we give you finished parts. You'll be flying in days, not weeks or months.

More performance...you wanted it, now you can have it!

Text and Photo from: http://www.quicksilveraircraft.com/sport.htm

MX Sport
Price: Not given

Rainbow Aircraft
Cheetah


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 109 kt | 125 mph | 201 kmh
Empty Weight: 274 kg | 604 lbs
MTOW Weight: 560 kg | 1235 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 260 ft | 80 m
Landing distance (50ft obstacle): 330 ft | 100 m

Aircraft information:
The Cheetah is the versatile 3-axis Microlight from Rainbow Aircraft, manufactured completetly in South Africa.

Note Landing and Take-off distance not over 50ft obstacle.

Photo and Text from: http://aerotrike.co.za

Cheetah
Price: Not given

Rand Robinson Engineering
KR-2S


Stall: 45 kt | 52 mph | 84 kmh
Cruise: 156 kt | 180 mph | 290 kmh
VNE: 174 kt | 200 mph | 322 kmh
Empty Weight: 209 kg | 460 lbs
MTOW Weight: 445 kg | 980 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 350 ft | 107 m
Landing distance (50ft obstacle): 600 ft | 183 m

Aircraft information:
The KR-2S is the latest KR in the fleet. It includes a 16 inch stretch in the fuselage over the standard KR-2, more head and leg room and pre-molds made of the latest oven-cured, vacuum-bagged pre-pregs. Its stylish raked canopy and fixed landing gear give it a racy appearance that is only exceeded by its performance. The KR-2S will accomodate engines including VW's, Subaru derivatives, Continental C-85's, and O-200's. Text and photo from: http://www.fly-kr.com/kr2s.htm

KR-2S
Price: Not given

Rans
S6 ES Coyote II


Stall: 31 kt | 36 mph | 58 kmh
Cruise: 94 kt | 108 mph | 174 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 273 kg | 602 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: 9:1
Take-off distance (50ft obstacle): 180 ft | 55 m
Landing distance (50ft obstacle): 250 ft | 76 m

Aircraft information:
The S-6ES went into production in April 1990. It is the second generation of the original S-6 design. Increased wing span through a fuselage re-design resulted in improved performance and appearance. The ES denotes "extended span". The design goals that the S-6 achieved represented a significant advance in quick-build kit planes. The S6ES series takes this goal even further. Using all prefinished parts and pre-sewn skins, the build time averages between 250 and 300 hours on the smaller engines. Coyote II's can be built in the confines of an average garage using normal shop tools and skills.

Note: Take-off and Landing distance is not over 50ft obstacle

Text from: www.rans.com

S6 ES Coyote II
Price: 14700 USD

Rans
S7


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 0 kg | 0 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:
The design of the S-7 originated out of the need to train Coyote I pilots; so the cockpit was set up the same with throttle left, stick in the middle. Named the Courier in honor of one of my favorite planes, The Helio Courier, the S-7 must have inherited some Helio spirit, since it also is very STOL.

Built with keeping-it-simple in mind the original plane weighed in at only 390 pounds with a 503 Rotax. It flew very well for the low horsepower, but soon was fitted to the 65 HP 532.

Over the years the basic plane stayed true to form, a light, simple plane, with traditional construction, minus the traditional headaches. However, in 2001 the S-7C, a much-refined version, was certified under the primary category. This plane represents 7 years of process to obtain the Type Certificate, and still has the performance and lines of the original 1985 S-7. In 2003 we introduced the S-7S, the kit form of the "C", and enjoy strong sales of this very much-refined fun flyer. The S-7S also complies with the new Sport Plane Rule, soon to take effect. Because the S-7S complies with the standards for sport planes we will be able to offer this plane in ready to fly form. Already we have begun production of these planes to meet the expected demand. For $69,000 you will be able to purchase a fully equipped S-7S, with such amenities, as Garmin moving map GPS/COM, and Transponder. The S-7S will be a practical plane as well as a fun sport plane. If you have the desire to build, the S-7S is a kit like few others. The level of detail to the manual, finish and quality of parts, and refined level of design will reinforce what a sound investment in sport flying the S-7S is. When completed you will have built your own version of our certified Courier.

Text from: www.rans.com

S7
Price: Not given

Rans
S-10 Sakota


Stall: 42 kt | 48 mph | 77 kmh
Cruise: 104 kt | 120 mph | 193 kmh
VNE: 113 kt | 130 mph | 209 kmh
Empty Weight: 231 kg | 510 lbs
MTOW Weight: 458 kg | 1010 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: 7:1
Take-off distance (50ft obstacle): 500 ft | 152 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
Rans S10 Sakota

ROTAX 582 65 HP liquid cooled with dual CDI ignition; RPM gauge; 2-Blade wood prop; 4130 Welded steel fuselage, tail group and tapered steel landing gear; Aluminum wheels with aircraft tires; Wheel pants; Pre-formed trussed wing ribs; .020 Aluminum leading edge wrap; 3" Tubular Aluminum Main spars; 2" Tubular Aluminum Aft spars; (2) 9 Gallon wing tanks; Seat adjustable in tilt and fore and aft; 2.7 ounce aircraft covering fabric, all tapes, glue, and inspection plates; Aluminum framed canopy; Airfoil struts; In-flight pitch trim; In-flight start; "Deep Set" panel; Roll over protection; Shoulder harnesses and lap belts; Dual elevator horns; 1 1/4" Push-pull elevator tube; Cable operated rudder; 3-Position flaps; Differential ailerons are cable and push-pull tube operated; Dual control sticks and throttles; Center flap lever; Pre-molded cowling; 12" Composite spinner; Heavy duty engine mount; Under the wing windows; Dual fuselage foot pegs and wing steps; Dual wire braced folding tail; Steerable tail wheel; Dual rudder pedals; Hydraulic brakes; Firewall sound proofing; Baggage compartment.

The S-10 Sakota is an FAA Approved 51% Kit - No welding required.

The Rans S-10 Sakota build Time: 350 to 600 hours

S-10 Sakota
Price: Not given

Rans
S-12S


Stall: 36 kt | 42 mph | 68 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 295 kg | 650 lbs
MTOW Weight: 522 kg | 1150 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 8:1
Take-off distance (50ft obstacle): 400 ft | 122 m
Landing distance (50ft obstacle): 400 ft | 122 m

Aircraft information:
The S-12S, "Super Airaile" is based off the highly successful S-12XL series. Changes made to the S-12S include a lower cabin and engine mount height. The result is less frontal area and a lower thrust line. Headroom is still more than adequate and will accommodate pilots up to 6’6". Dacron coverings were replaced with traditional dope and fabric. To adapt the new covering system, mods to the wing and tail included new ribs all around, plus leading edge wraps for the wing. The total effect of the mods brought about an increase in cruise, climb, glide ratio, and a lower stall. In the air the handling is improved in both roll and yaw.

Build time for the Super Airaile will be on the average 200 to 300 hours more than the XL, but still within reason. Most builders should complete the plane in 6 to 12 months. This is due to the tremendous amount of pre-fabrication and precise fit of our parts. Quality airtime is built around a kit that is de- signed to be built by the first time builder; this is where the S-12S excels. A good manual is at the center of fast build times, and as with our airframes the manuals are also "test flown". Our Tech Staff is always assembling our own product to keep the manuals up to date.

Text and photo from: http://www.rans.com/

S-12S
Price: Not given

Rans
S-12XL Airaile


Stall: 29 kt | 33 mph | 53 kmh
Cruise: 65 kt | 75 mph | 121 kmh
VNE: 87 kt | 100 mph | 161 kmh
Empty Weight: 215 kg | 475 lbs
MTOW Weight: 442 kg | 975 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: 7:1
Take-off distance (50ft obstacle): 400 ft | 122 m
Landing distance (50ft obstacle): 400 ft | 122 m

Aircraft information:
The S-12XL Airaile went into production in March of 1990 and has enjoyed a progressive evolution. Improvements to cabin comfort, durability, and performance are the direct result of working with user input. This is typical of the Airaile program from the beginning. The Airaile was designed to fulfill many foreign and domestic requests for a two-place pusher with side-by-side seating that was economical to buy, quick to build, easy to fly, and rugged enough to withstand the rigors of training. Over the years, the Airaile has earned a respected position in over 40 countries as the plane capable of fulfilling these goals. Typical of RANS aircraft, the Airaile only requires a two-car garage and common shop tools and skills to complete from start to finish.

Text and photo from: http://www.rans.com/s-12xl.htm

S-12XL Airaile
Price: Not given

RANS
S-6ES COYOTE II


Stall: 30 kt | 34 mph | 55 kmh
Cruise: 83 kt | 95 mph | 153 kmh
VNE: 96 kt | 110 mph | 177 kmh
Empty Weight: 240 kg | 530 lbs
MTOW Weight: 467 kg | 1030 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: 9:1
Take-off distance (50ft obstacle): 160 ft | 49 m
Landing distance (50ft obstacle): 250 ft | 76 m

Aircraft information:
- A VERY NICE AIRCRAFT TO FLY

S-6ES COYOTE II
Price: Not given

Remos Aircraft GmbH
G-4 Velocity


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 124 kt | 143 mph | 230 kmh
VNE: 151 kt | 174 mph | 280 kmh
Empty Weight: 290 kg | 639 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1300 ft/min | 6.5 m/s
Glide Ratio: 17:1
Take-off distance (50ft obstacle): 450 ft | 137 m
Landing distance (50ft obstacle): 480 ft | 146 m

Aircraft information:
Photo and text from: http://www.remos.com/de/Beginn.htm

G-4 Velocity
Price: Not given

Remos Aircraft GmbH
G-3 Mirage


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 121 kt | 140 mph | 225 kmh
Empty Weight: 129 kg | 285 lbs
MTOW Weight: 214 kg | 472 lbs
Climb Ratio: 1300 ft/min | 6.5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 450 ft | 137 m
Landing distance (50ft obstacle): 450 ft | 137 m

Aircraft information:
G3

Text and photo from: http://www.remos.com/de/Beginn.htm

G-3 Mirage
Price: Not given

RMT Aviation
Bateleur 115 T


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 149 kt | 171 mph | 276 kmh
VNE: 173 kt | 199 mph | 320 kmh
Empty Weight: 259 kg | 570 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1700 ft/min | 9 m/s
Glide Ratio: 18
Take-off distance (50ft obstacle): 500 ft | 152 m
Landing distance (50ft obstacle): 400 ft | 122 m

Aircraft information:
The Bateleur and its many Commercial Applications

The unusual configuration of the Bateleur brings numerous advantages compared to the conventional high or low winged aircraft. (Most modern military attack aircraft use a similar concept). Its flight and handling characteristics remaining totally standard allows any pilot instant conversion. The tandem seating for 2 people gives both pilot and passenger full view to both sides. The up front seated person (normally the pilot) has a view only comparable with that of a helicopter with no obstruction through wings. The Bateleur is capable of performing most tasks of the Helicopter but with some significant advantages and with a saving of more than 90% both in purchase price and airborne expense. The concept has proven to be more stable in severe turbulence, comparable only to aircraft many times its weight making it very suitable as an aerial photographic or observation platform. It’s endurance and range in excess of 7 hours / 1000 Km can be extended with auxiliary tanks by another 50%.

Text and photo from www.rmtaviation.com

Bateleur  115 T
Price: 92800 EURO

RMT Aviation
Bateleur 912 S


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 140 kt | 162 mph | 260 kmh
VNE: 173 kt | 199 mph | 320 kmh
Empty Weight: 250 kg | 551 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 1400 ft/min | 7.1 m/s
Glide Ratio: 18
Take-off distance (50ft obstacle): 720 ft | 220 m
Landing distance (50ft obstacle): 490 ft | 150 m

Aircraft information:
www.rmtaviation.com As Ultralight MTOW is 450 kg

Bateleur 912 S
Price: 78800 EURO

Rolandas Kalinauskas
RK - 6


Stall: 32 kt | 37 mph | 59 kmh
Cruise: 84 kt | 96 mph | 155 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 550 kg | 1213 lbs
Climb Ratio: 1300 ft/min | 6.5 m/s
Glide Ratio: 14
Take-off distance (50ft obstacle): 160 ft | 50 m
Landing distance (50ft obstacle): 230 ft | 70 m

Aircraft information:
More information about RK series planes at http://avia.tinklapis.lt or povilas_k@one.lt

RK - 6
Price: 35000 EURO

Rolandas Kalinauskas Aircraft
RK-7


Stall: 32 kt | 37 mph | 59 kmh
Cruise: 84 kt | 96 mph | 155 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 250 kg | 551 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 14
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Engine and Avionics are not included.

RK-7
Price: 15000 EURO

Rotec Engineering Inc
Rotec Rally


Stall: 17 kt | 20 mph | 32 kmh
Cruise: 30 kt | 35 mph | 56 kmh
VNE: 48 kt | 55 mph | 89 kmh
Empty Weight: 103 kg | 228 lbs
MTOW Weight: 215 kg | 475 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:
An early ultralight aircraft.

Photo and info from http://www.ultralightnews.com/antulbg/rotecrally_ultralight.htm

Rotec Rally
Price: Not given

S.A.I
G97 Spotter


Stall: 31 kt | 36 mph | 58 kmh
Cruise: 95 kt | 109 mph | 176 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 530 kg | 1168 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
S.A.I. Società aeronautica Italiana s.r.l. (Italian aeronautical society Ltd)

Photo from http://www.saiaeronautica.com/indexuk.htm

G97 Spotter
Price: Not given

SAB
D-20


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 100 kt | 115 mph | 185 kmh
VNE: 157 kt | 180 mph | 290 kmh
Empty Weight: 290 kg | 639 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1100 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 720 ft | 220 m
Landing distance (50ft obstacle): 720 ft | 220 m

Aircraft information:
AeroConsult GSM 00 33(0) 677 184 096 contact@aeroconsult.fr www.aeroconsult.fr

D-20
Price: 85000 EURO

Sankara Holdings
Aliseo Flying Boat


Stall: 24 kt | 28 mph | 44 kmh
Cruise: 40 kt | 46 mph | 74 kmh
VNE: 75 kt | 86 mph | 139 kmh
Empty Weight: 218 kg | 480 lbs
MTOW Weight: 445 kg | 980 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 9:1
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 150 ft | 46 m

Aircraft information:
The most sophisticated and powerfull flying boat available today. The best airplane sold for the mega-yacht market. LSA.

Aliseo Flying Boat
Price: 34000 USD

SAUPER - AVIATION
PAPANGO ULM


Stall: 31 kt | 36 mph | 57 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 124 kt | 143 mph | 230 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 990 ft/min | 5 m/s
Glide Ratio: 10
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 390 ft | 120 m

Aircraft information:
www.sauper-aviation.com

PAPANGO ULM
Price: 50170 EURO

SAUPER - AVIATION
J300 JOKER


Stall: 30 kt | 34 mph | 55 kmh
Cruise: 76 kt | 87 mph | 140 kmh
VNE: 107 kt | 123 mph | 198 kmh
Empty Weight: 275 kg | 606 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 7
Take-off distance (50ft obstacle): 560 ft | 170 m
Landing distance (50ft obstacle): 490 ft | 150 m

Aircraft information:
www.sauper-aviation.com info@sauper-aviation.com

J300  JOKER
Price: 40000 EURO

Seahawk Industries
Condor


Stall: 22 kt | 25 mph | 40 kmh
Cruise: 30 kt | 35 mph | 56 kmh
VNE: 56 kt | 65 mph | 105 kmh
Empty Weight: 106 kg | 234 lbs
MTOW Weight: 215 kg | 475 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 Condor is a single seat, high wing, wire braced ultralight, featuring a tri-cycle landing gear suspension system.

The control system is conventional stick and rudder, with spoilerons on the wings for aiding in roll control.

The plane is has a single surface wing, and is wire braced. The kit came as a simple bolt together assembly taking approximately 75 hours to assemble.

The Condor single was powered by Kawasaki 440 engines, with some of the two seaters equipped with Kawasaki liquid cooled engines of 80 hp.

The Condor single place and two place were produced up until about 1984.

Photo and text from: http://www.ultralightnews.com/antulbg/condor_ultralight.htm

Condor
Price: Not given

Silence Flugzeugbau GmbH
Silence Twister


Stall: 41 kt | 47 mph | 76 kmh
Cruise: 127 kt | 146 mph | 235 kmh
VNE: 162 kt | 186 mph | 300 kmh
Empty Weight: 238 kg | 525 lbs
MTOW Weight: 399 kg | 880 lbs
Climb Ratio: 1275 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:
Have you ever dreamed of flying a Spitfire? If the answer is 'yes', you should take a look at the new Silence, manufactured by Silence Aircraft in Verl near Bielefeld, Germany. With this aircraft, you get all the fun and good looks of the Spitfire on a micro light budget!

Text and photo from: http://www.silence-flugzeugbau.de

Silence Twister
Price: Not given

Sky-Maxx Manufactory
SKY-MAXX


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 139 kt | 160 mph | 258 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 750 kg | 1653 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 100 ft | 30 m
Landing distance (50ft obstacle): 100 ft | 30 m

Aircraft information:
Available: Several editions (tropical, desert, photography) "Ready for fly" or as a kit More info: http://www.sky-maxx.com

SKY-MAXX
Price: 95000 USD

Skyfox Aviation
Skyfox


Stall: 43 kt | 49 mph | 80 kmh
Cruise: 70 kt | 81 mph | 130 kmh
VNE: 93 kt | 107 mph | 172 kmh
Empty Weight: 315 kg | 694 lbs
MTOW Weight: 520 kg | 1146 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 390 ft | 120 m

Aircraft information:
Skyfox

Data: http://www.skyfox.net.au
Photo: http://www.holbrookultralightclub.asn.au/

Skyfox
Price: Not given

Skystar
Kitfox


Stall: 31 kt | 36 mph | 58 kmh
Cruise: 70 kt | 81 mph | 130 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 233 kg | 514 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 330 ft | 100 m

Aircraft information:
The Series 7 is for serious pilots that demand performance, comfort, and most of all safety. With a useful load of up to 800 pounds, 28 gallon fuel capacity, 150 pound cargo capacity and STOL performance it’s just waiting to take you where most planes can only dream about, it’s no wonder that it’s known as a Jeep with wings. Having a wide cockpit, folding wings, able to convert from tailwheel to nose wheel in a matter of hours makes the Series 7 extremely versatile.

With thousands sold all over the world the Classic 4 has evolved over the last 20 years to become the icon of the Kitfox. 4130 chromoly tubing structure, folding wings, multiple engine, cowling, and landing gear choices. The Classic 4 is the most copied kitbuilt on the market today.

Kitfox
Price: Not given

Slip Stream International
Genesis


Stall: 41 kt | 47 mph | 76 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 295 kg | 650 lbs
MTOW Weight: 590 kg | 1300 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 350 ft | 107 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
GENESIS...according to Webster, "the origin, or coming into being". An appropriate name for a design as innovative and original as the flagship of the SlipStream pusher line of aircraft kits. Originally designed and prototyped in 1992, the GENESIS has been hailed by the industry for its performance, flight characteristics and sexy styling.

The GENESIS is the answer for the pilot who wants a modern, two-place, roomy, side-by-side aircraft for a price below that of a 30-year old Cessna. Available with your choice of dual yoke controls or center stick, the GENESIS can be configured to satisfy your exacting requirements. Equipped with the standard Rotax 582, and in solo configuration, take-off roll is a mere 100 feet, with a 250 foot landing roll and a climb rate of 1,000 fpm. The GENESIS base price also includes dual 10-gallon wing tanks to provide for four hours of cross-country endurance.

Thinking about a floatplane? Try on a pair of the all new "Shark Series" amphibious floats and you've opened the door to unbelievable adventure. Computer designed to reduce drag and to provide for rapid hydroplaning, the "Shark Series" floats are built to withstand impacts in excess of 3,000 lbs. per square inch and are rated for up to 1,600 lbs. Coupled with the GENESIS and any of the larger Rotax engines, this floatplane combination will take you to destinations others only dream about.

Worried about useful load? Don't be! With an average empty weight of 565 lbs., the GENESIS equipped with the standard Rotax 582 has a useful load of 635 lbs. Purchase any of the larger optional powerplants, and the gross weight capability increases to 1400 lbs., providing for an even larger useful load. Still not enough? The all new HD option is the answer, with a "beefed up" airframe capable of safely carrying up to 1600 lbs. and an unbelievable useful load envelope of over 800 lbs.! We have tested and proven all of our offered engine options, so your choice is limited only by your performance requirements and available budget.

In terms of build time the GENESIS typically will take about 400 hours to complete, and that's about as low as you'll find for a real enclosed cabin aircraft. All of the welding and fabrication is done before the kits leave our plant, and our manuals are clearly written with easy step by step instructions, and numerous photos, illustrations and CAD drawings, so even a novice builder can be up and flying in no time.

The GENESIS airframe lists for $11,073*, and includes all of the flight surfaces, fuselage, fiberglass enclosure, landing gear, wheels and tires, control system and doors. Among the many options we offer are custom hydraulic brakes, cabin heating, floats, wheel pants, strut fairings, complete instruments packages, and finishing systems (we are a Randolph Products distributor). As a basis of comparison, a complete Genesis aircraft, ready to fly, typically runs from $21,000 to $32,000, depending on your powerplant and choice of options.

Whether you are seriously looking for the aircraft of your dreams, or just kicking tires, please phone, fax, or email us and we will be happy to answer any questions you may have. Why settle for a 30-year-old aircraft when you can have today's styling, performance, handling, and all around excitement at an affordable price?

Text and Photo from: http://www.slipstream.bz

Note: Take-off distance not over 50ft obstacle.

Genesis
Price: 11073 USD

Sonex Ltd.
Sonex


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 113 kt | 130 mph | 209 kmh
VNE: 171 kt | 197 mph | 317 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 330 ft | 100 m
Landing distance (50ft obstacle): 490 ft | 150 m

Aircraft information:
Photo from http://www.sonex-ltd.com/photo_archive.html

Sonex
Price: Not given

Sonex Ltd.
Xenos


Stall: 36 kt | 42 mph | 68 kmh
Cruise: 104 kt | 120 mph | 193 kmh
VNE: 167 kt | 192 mph | 309 kmh
Empty Weight: 284 kg | 626 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:
Sonex Xenos

More information and picture from: http://www.sonex-ltd.com/waiex.html

Xenos
Price: Not given

Sonex Ltd.
Waiex


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 113 kt | 130 mph | 209 kmh
VNE: 171 kt | 197 mph | 317 kmh
Empty Weight: 263 kg | 580 lbs
MTOW Weight: 522 kg | 1150 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 400 ft | 122 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
V-tail

Waiex
Price: Not given

Storch Aviation Serbia
Slepcev Microlight Storch


Stall: 22 kt | 25 mph | 41 kmh
Cruise: 72 kt | 83 mph | 133 kmh
VNE: 80 kt | 92 mph | 148 kmh
Empty Weight: 289 kg | 637 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 30 ft | 9 m
Landing distance (50ft obstacle): 30 ft | 9 m

Aircraft information:
Ultralight STOL aircraft, 3/4 replica of Fieseler Fi-156 Storch. Avaliable ready to fly or as a kit

Slepcev Microlight Storch
Price: 45000 EURO

Storm Aircraft
Rally


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 107 kt | 123 mph | 198 kmh
VNE: 145 kt | 167 mph | 269 kmh
Empty Weight: 345 kg | 760 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1200 ft/min | 6,5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
-

Rally
Price: Not given

Storm Aircraft
Century


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 121 kt | 140 mph | 225 kmh
VNE: 167 kt | 193 mph | 310 kmh
Empty Weight: 290 kg | 639 lbs
MTOW Weight: 600 kg | 1323 lbs
Climb Ratio: 1200 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:
Text and photo from http://www.aireliteaviation.com

Century
Price: Not given

Summit Powered Parachutes
Summit SS (single seat)


Stall: 0 kt | 0 mph | 0 kmh
Cruise: 30 kt | 35 mph | 56 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 106 kg | 233 lbs
MTOW Weight: 249 kg | 550 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 100 ft | 30 m

Aircraft information:
In 1999, at the Sun n Fun airshow in Florida, the Summit II made its debut and we have never looked back since.

The uniqueness of the Summit created a real interest and we had many people comment on how different our kit was then anything they had ever seen in the market. They were right!!!. We had incorporated in our very unique design, a true two seat placement that allowed pilot and passenger to sit in their own separate seats for the most comfortable arrangement. We had a single fuselage tube that had every attach point triangulated, we had a slider foot control system for ease of canopy steering, we had stainless steel rails around the pilot and passenger for maximum protection, we had a four point pick up system for our risers for the best control against any pendulum affect and above that, all the kits were anodized which was superior to the typical powder coating. Our landing gear was designed so that it was back under the engine so that in the event of a hard landing, the wheels would touch first, not the protective propeller guard thus eliminating a lot of the problems with broken propeller blades that plagued our competitors.

Text and Photo from: http://www.summitppc.com

Summit SS (single seat)
Price: Not given

Sundog Powerchutes Inc
Two-Seater Powered Parachute


Stall: 0 kt | 0 mph | 0 kmh
Cruise: 29 kt | 33 mph | 53 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 152 kg | 336 lbs
MTOW Weight: 222 kg | 489 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 5:1
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 100 ft | 30 m

Aircraft information:
Sundog Powerchutes

Weather you call it a paraplane, powered para plane, parachute plane, motorized parachute, flying parachute, power parachute, PPC, UFO, big bird, or ultra light high flying fangled contraption, it still amounts to a lot of great flying fun, and that's what our company is all about. Sundog Powerchutes Inc. - Sundog Powered Parachutes, is a powered parachute manufacturer of a unique new design of powered parachutes. Our side by side powered parachute model is what we specialize in and what really sets us apart from most of the other powered parachute manufacturers, but we also manufacture a single seater as well. We have a nice selection of powered parachute pictures, and even a couple of powered parachute videos in our gallery section to give you a better idea of what this sport is all about.

Photo and text from: http://www.sundogpowerchutes.com

Two-Seater Powered Parachute
Price: 15995 USD

Taylorcraft
Taylor Cub


Stall: 37 kt | 43 mph | 69 kmh
Cruise: 87 kt | 100 mph | 161 kmh
VNE: 129 kt | 148 mph | 238 kmh
Empty Weight: 404 kg | 890 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 750 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 700 ft | 213 m
Landing distance (50ft obstacle): 625 ft | 191 m

Aircraft information:
Text and photo from www.taylorcraft.com

Taylor Cub
Price: Not given

Tecnam
P92 Echo


Stall: 33 kt | 38 mph | 61 kmh
Cruise: 105 kt | 121 mph | 195 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 281 kg | 619 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1260 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 330 ft | 100 m

Aircraft information:
photo by Daniel Mattson

Other info: www.tecnam.com

P92 Echo
Price: Not given

Tecnam
P96 Golf


Stall: 33 kt | 38 mph | 61 kmh
Cruise: 116 kt | 133 mph | 215 kmh
VNE: 140 kt | 161 mph | 259 kmh
Empty Weight: 281 kg | 619 lbs
MTOW Weight: 550 kg | 1213 lbs
Climb Ratio: 1180 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 590 ft | 180 m
Landing distance (50ft obstacle): 328 ft | 100 m

Aircraft information:
Tecnam P96 Golf. Air navigation standards. Wing structure features a single spar torque box connected to fuselage via three pin attachments to each half wing.

Fuselage structure is a steel tubing framework for cabin area high protection and semi-monococque light alloy tail to support empennage. Ease of inspection; immediate access for servicing that is efficient and inexpensive at the same time. Particular attention is devoted to fuselage aerodynamics with the adoption of a composite fairing that elegantly and efficiently joins the cabin with the vertical tail.

Specially studied wheel fairing are mounted on each wheel to reduce parasite drag. Landing light is located inside engine cowling in correspondence of nose wheel strut.

Engine cowling is made up two parts and allows for quick and complete opening. Fuel tanks are integral part of the wing structure and feature 35 litre capacity per each half wing. Fuel feed is via an engine driven pump and is backed-up for emergency by an electric pump.

The wide cabin (1,10 m) features two side by side seats that can be adjusted via sliding rail stops, a large baggage compartment is located behind seats.

Cabin access is through a canopy that slides towards rear of aircraft overlapping tail fairing consequently allowing unrestricted opening even with aircraft in flight.

The wide windshield offers a complete view unhindered by structural elements, while large side windows allow for excellent visibility.

The entirely moving tailplane permits superior control and a high degree of stick free stability, moving surfaces feature mass balancing.

Landing gear components have been thoroughly tested and feature a clear record of safety and efficiency. The main landing gear consists of special steel springs with 5.00-5 size tires and hydraulically actuated disc brakes, while nose gear features a steerable wheel with rubber shock.

Instrument panel meets General Aviation standards both in size and quality allowing for installation of a wide variety of flight instrumentation inclusive of IFR, engine controls and com/nav apparatus.

Flight controls are traditional type with dual stick, dual rudder pedals and dual throttle knobs on dashboard. Longitudinal trim and electrical flap controls with position indicators are also located on dashboard.

Cabin ventilation is via adjustable air vents fed via buried scoops.

The Text and photo from www.tecnam.com

P96 Golf
Price: Not given

Tecnam
P2004 Bravo


Stall: 38 kt | 44 mph | 70 kmh
Cruise: 116 kt | 133 mph | 215 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 331 kg | 730 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 762 ft | 232 m
Landing distance (50ft obstacle): 610 ft | 186 m

Aircraft information:
-

P2004 Bravo
Price: Not given

Tecnam
P2002 Sierra


Stall: 38 kt | 44 mph | 70 kmh
Cruise: 116 kt | 133 mph | 215 kmh
VNE: 135 kt | 155 mph | 250 kmh
Empty Weight: 331 kg | 730 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 762 ft | 232 m
Landing distance (50ft obstacle): 610 ft | 186 m

Aircraft information:
-

P2002 Sierra
Price: Not given

TeST
TST-10 M


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 57 kt | 65 mph | 105 kmh
VNE: 97 kt | 112 mph | 180 kmh
Empty Weight: 205 kg | 452 lbs
MTOW Weight: 300 kg | 661 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: 40
Take-off distance (50ft obstacle): 1180 ft | 360 m
Landing distance (50ft obstacle): 750 ft | 230 m

Aircraft information:
TST-10 ATLAS M is a self-launching UL glider with electric retractable power plant controlled by electronic system

Photo and Text from: http://www.test.infoline.cz/

TST-10 M
Price: 22900 EURO

The Little Aeroplane Comapny
Sherwood Ranger


Stall: 56 kt | 65 mph | 105 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 700 ft | 213 m
Landing distance (50ft obstacle): 800 ft | 244 m

Aircraft information:
The Sherwood Ranger is a lightweight two seat open cockpit biplane, designed to reduce the cost of owning and operating your own aeroplane to the absolute minimum. One of its major features is that the wings can be folded and the aeroplane loaded onto a trailer in less than three minutes, thus eliminating hangarage costs by allowing the aeroplane to be stored at home. Landing fees are unnecessary because the superb performance and handling characteristics allow safe operation from unprepared grass fields as short as 250yds. The rugged construction coupled with classic timeless styling, ensures that well maintained examples will hold their resale value indefinitely.

Photo and Information from: http://www.talla3.com/tlac.nsf/

Sherwood Ranger
Price: Not given

The New Kolb Aircraft
Mark III Xtra


Stall: 36 kt | 41 mph | 66 kmh
Cruise: 78 kt | 90 mph | 145 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 249 kg | 550 lbs
MTOW Weight: 454 kg | 1000 lbs
Climb Ratio: 1100 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 200 ft | 61 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
www.tnkolbaircraft.com

Mark III Xtra
Price: 18700 USD

The New Kolb Aircraft
Sport 600


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 120 kt | 138 mph | 222 kmh
VNE: 135 kt | 155 mph | 249 kmh
Empty Weight: 295 kg | 650 lbs
MTOW Weight: 599 kg | 1320 lbs
Climb Ratio: 1350 ft/min | 7 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 500 ft | 152 m
Landing distance (50ft obstacle): 500 ft | 152 m

Aircraft information:
www.tnkolbaircraft.com

Sport 600
Price: 68000 USD

The New Kolb Aircraft
Firestar II


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 61 kt | 70 mph | 113 kmh
VNE: 74 kt | 85 mph | 137 kmh
Empty Weight: 147 kg | 325 lbs
MTOW Weight: 329 kg | 725 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 250 ft | 76 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
www.tnkolbaircraft.com

Firestar II
Price: 9000 USD

Thunderbird Aviation
Hiperlight SNS-9


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 74 kt | 85 mph | 137 kmh
VNE: 98 kt | 113 mph | 182 kmh
Empty Weight: 163 kg | 360 lbs
MTOW Weight: 369 kg | 814 lbs
Climb Ratio: 600 ft/min | 3 m/s
Glide Ratio: 12:1
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
Hiperlight an interesting looking light aircraft!

Photo from http://www.hiperlightaircraft.com

Note: Take-off and landing distance not over 50ft obstacle

Hiperlight SNS-9
Price: 24900 USD

Titan Aircraft Company
T-51 Mustang


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 130 kt | 150 mph | 241 kmh
VNE: 171 kt | 197 mph | 317 kmh
Empty Weight: 386 kg | 850 lbs
MTOW Weight: 658 kg | 1450 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 300 ft | 91 m

Aircraft information:
Titan Aircraft is proud to introduce the T-51 Mustang, the newest addition to our family of light aircraft. The T-51 Mustang is a two-seat, dual control, tandem seat aircraft. It can be built as an N-numbered amateur built experimental aircraft or as a Light Sport Aircraft. The T-51 Mustang incorporates material and systems not commonly found in aircraft comparably priced. This, combined with Titan Aircraft’s renowned reputation for high quality products, superior aircraft performance, and outstanding customer support, is sure to provide the pilot and kit builder a very pleasurable experience.

The kit has an estimated build time of 600 hours and includes all required material, components and fasteners. The kit does not however include the engine, propeller and instruments because of different customer preferences. When equipped with the Rotax 912S engine, controllable propeller, and a full compliment of necessary flight instruments; we expect the finished T-51 to cost well under $55,000.00.

Titan Aircraft is providing a replica P-51 Mustang that combines friendly low speed handling characteristics with agility and high performance. The T-51 Mustang is rated at a +6g / -4g load limit capability at a gross weight of 1450 pounds. When operating with the 912S engine and landing gear retracted the cruise speed is 150mph. The stall speed in landing configuration is 39mph.

Text and Photo from: http://www.titanaircraft.com

Note: Take-off and landing distance not over 50ft obstacle.

T-51 Mustang
Price: 37500 USD

Titan Aircraft Company
Tornado II


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 96 kt | 110 mph | 177 kmh
VNE: 130 kt | 150 mph | 241 kmh
Empty Weight: 200 kg | 440 lbs
MTOW Weight: 454 kg | 1000 lbs
Climb Ratio: 1600 ft/min | 8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 250 ft | 76 m

Aircraft information:
The Titan Tornado 2 incorporates material and systems not commonly found in aircraft comparably priced. This, combined with Titan Aircraft’s renowned reputation for high quality product, superior aircraft performance and outstanding customer support, is sure to provide the pilot and kit builder a very pleasurable experience, and a fantastic resale value. The kit has an estimated build time of 150 - 300 hours and includes all required material, components and fasteners. The kit does not however include the engine, propeller, and instruments because of different customer preferences. This aircraft combines friendly low speed handling characteristics with agility and high performance. The Titan Tornado 2 is designed to a +6g / -4g load limit capability at 1000 pounds gross weight. When operating with the rotax 582 engine the cruise speed is in excess of 110 mph. The stall speed in landing configuration flying solo is 35 mph. We invite inquiries.

Text and Photo from: http://www.titanaircraft.com

Note: Take-off and landing distance not over 50ft obstacle

Tornado II
Price: Not given

TL ULTRALIGHT
TL 22 DUO / ESO


Stall: 23 kt | 26 mph | 42 kmh
Cruise: 38 kt | 43 mph | 70 kmh
VNE: 65 kt | 75 mph | 120 kmh
Empty Weight: 130 kg | 287 lbs
MTOW Weight: 360 kg | 794 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: 9.5:1
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
photo from: http://www.tl-ultralight.cz/

TL 22 DUO / ESO
Price: Not given

TL ULTRALIGHT
TL-2000 STING CARBON


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 130 kt | 149 mph | 240 kmh
VNE: 165 kt | 190 mph | 305 kmh
Empty Weight: 275 kg | 606 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1600 ft/min | 8 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:
TL-2000 Sting Carbon is the latest generation from the TL-ULTRALIGHT Company. The TL-2000 Sting Carbon offers a ground breaking optional in flight adjustable propeller witch is electronically controlled needing no pilot input normally only available on aircraft costing hundreds of thousands.

The Whole Aicraft is made from Carbon Fibre. The elegant and perfectly aerodynamically shaped TL-2000 Sting was designed to achieve the highest speed of flight. The TL-2000 Sting Carbon really is the fastest Czech Ultralight and its maximum speed in horizontal flight of about 285 km/h and its not definitely the last word. Interresting is also speed of flight from minimum 63 km/h to insuperable speed 305 km/h which gives pilots of all abilities the opportunity to operate within their skill levels and to fly from grass strips or tarmac.

In a pilot´s hands the TL-2000 Sting Carbon is a dynamic machine with the characteristics and comfort of a much larger aircraft. The panoramic view and low noise levels give you a level of comfort and style as yet unattainable.

To aid your comfort an optional cabin heater can be installed. The TL-2000 Sting Carbon two seat, side by side cabin is very roomy even for the fuller figure.

All control and flight instruments have been ergonomically positioned to maximise ease of use even when securely strapped in.

The aircraft is fitted with double steering and standard nose wheel configuration with the two main wheels being disc braked and a durable nose wheel. The buoyancy flaps is possible to extend in two position. One is for taking off 15 oC and the other one for landin 35 oC.

The very latest in construction techniques enable a strong light and durable aircraft to be produced. If you need to take your STING home, you can remove the wings easily in 10 minutes. The TL-STING is equipped with ROTAX 912, 912 S or 914 in a accordance with our customer. Also there are many types and construction of propellers. We can offer a wide choice of Avionic, GPS, and rescue systems to suit your own specification.

Text and Photo from: http://www.tl-ultralight.cz/

TL-2000 STING CARBON
Price: Not given

TL ULTRALIGHT
TL-232 Condor Plus


Stall: 32 kt | 37 mph | 60 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 97 kt | 112 mph | 180 kmh
Empty Weight: 280 kg | 617 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 800 ft/min | 4,6 m/s
Glide Ratio: 1:14
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
Condor TL232 Plus is further development of previous well-proven TL-132 Condor. It is a two-place ultralight airplane of latest generation with seats side-by-side in roomy and comfortable cockpit. The seats are adjustable and have inclinable backrests.

TL-232 Condor Plus
Price: Not given

TL ULTRALIGHT
TL-96 STAR


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 108 kt | 124 mph | 200 kmh
VNE: 148 kt | 171 mph | 275 kmh
Empty Weight: 288 kg | 635 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1200 ft/min | 6 m/s
Glide Ratio: 15:1
Take-off distance (50ft obstacle): 890 ft | 270 m
Landing distance (50ft obstacle): 980 ft | 300 m

Aircraft information:
The all composite TL-96 Star is the predessor of TL-2000 Sting.Star is made of glass fiber whereas carbon is being used in Sting's manufacturing.

TL-96 STAR
Price: 56000 EURO

TL ULTRALIGHT
TL-32 Typhoon


Stall: 23 kt | 26 mph | 42 kmh
Cruise: 67 kt | 78 mph | 125 kmh
VNE: 76 kt | 87 mph | 140 kmh
Empty Weight: 272 kg | 600 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:
The company TL Ultralight was established in 1990 in Hradec Králové as a firm for development and production of trike and afterwards for ultralight aircrafts. The company started with production of trike TL 1 and TL 2 which is very succesful and it has been still selling all around the world. In 1991 the Ultralight company started with production of TL 32 Typhoon, this type of ultralight aircraft became popular for recreation flying.We had produced over 300 pieces of this kind of aircraft, which you can still see them flying all around the Europe and the USA. Nowadays this aircraft is not build anymore. This type of aircraft was followed by TL 132 CONDOR. This aircraft has been built according to strict criterion of fly schools and experienced private pilots. In the same way was produced TL 232 CONDOR. This ultralight airplane has certification in Germany, France, Holland, Spain ….etc. We have already sold over 280 pieces and it has been still succesfuly selling. Another great refreshing airplane of the market was the trike TL 22 DUO. In 1996 company has started with development of complete new type – TL 96 STAR. This progress took 2 years and it meant transition to complete new materials and technology. This aircraft create TL Ultralight´s main produce program. It is certificated in many countries as Germany, Spain, Italy, Benelux… In these days company is producing 4 aircrafts a month to complete satisfaction to all our customers.

TL-32  Typhoon
Price: Not given

TMM-Avia
T-10 Frigate


Stall: 33 kt | 39 mph | 62 kmh
Cruise: 81 kt | 93 mph | 150 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 315 kg | 694 lbs
MTOW Weight: 550 kg | 1213 lbs
Climb Ratio: 1200 ft/min | 6,2 m/s
Glide Ratio: 11
Take-off distance (50ft obstacle): 360 ft | 110 m
Landing distance (50ft obstacle): 230 ft | 70 m

Aircraft information:
T-10 is a very light multipurpose aircraft, intended for different aviation tasks: pilot training, crop spraying, aerial patroing and monitoring. The airplane's fugelage frame work has truss structure, made of stainless steel.Wingtips(double spar,all wooden) and horizontal empennage are foldable along the fuselage,wchich markedly facilitates the airplane's assembly, disassembly, transportation and storage. T-10 tricycle non-retractable landing gear, enables it to operate from ground, grass and paved runways. The T-10's design makes all provisions for the crew salvation in emergency situations, flight safety at low altitudes, maintainability and repairability.As additional option it can be equipped with a Cobra recovery system. We propose the T-10 Frigate as a ready-to-fly airplane or as a kit(21 600 euro)!

T-10 Frigate
Price: 42500 EURO

Tomas Podesva
Trener Baby


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 113 kt | 130 mph | 210 kmh
Empty Weight: 296 kg | 653 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 400 ft/min | 2,5 - 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 980 ft | 300 m
Landing distance (50ft obstacle): 980 ft | 300 m

Aircraft information:
Replica of the czech ZLin 126 Trener; manufacturers homepage: www.podesva-air.com

Trener Baby
Price: 47000 EURO

Tomi Aviation
Tomi Cross 5,1 / MW 155 VingeTrike


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

Aircraft information:
-

Tomi Cross 5,1 / MW 155 VingeTrike
Price: 15000 EURO

U.S. Light Aircraft Corp.
Hornet


Stall: 28 kt | 32 mph | 51 kmh
Cruise: 61 kt | 70 mph | 113 kmh
VNE: 104 kt | 120 mph | 193 kmh
Empty Weight: 454 kg | 1000 lbs
MTOW Weight: 215 kg | 475 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: 9:1
Take-off distance (50ft obstacle): 175 ft | 53 m
Landing distance (50ft obstacle): 150 ft | 46 m

Aircraft information:
U.S. Light Aircraft Corp. Hornet

The entire airframe is completed by the factory, assembled in precise factory jigs, with over 7,000 rivets.

The Hornet components are manufactured by computer automated equipment, especially designed by U.S.L.A.C. to produce the most precise, highest-quality aircraft possible.

Since its introduction in ’93, Hornet builders have won an unprecedented number of awards at the largest air shows in the nation - more than any single design in its class.

Air shows are judged by E.A.A. judges, skilled in all phases of aircraft construction, and are familiar with the "latest and greatest" the world has to offer. These judges know quality when they see it.

Text and Photo From: www.flyhornet.com

Note: take-off and landing distance not over 50ft obstacle

Hornet
Price: 18950 USD

Ulbi
Wild thing WT01 / WT02


Stall: 30 kt | 35 mph | 56 kmh
Cruise: 76 kt | 87 mph | 140 kmh
VNE: 108 kt | 124 mph | 200 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 0 kg | 0 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:
Since 1997 the "Wild Things" have been finished in the versions WT 01 and WT 02 at the Aerodrome Haßfurt (EDQT). As the general importer of Jabiru in Germany we have aircrafts and engines of the Australian company in our program. Thus we are partner for maintanance, repairs and sales as well as for technical support. Because of the very strong and approved construction made of aluminum the Wild Thing is the ideal partner for - Bushpilots - Explorers. But it is also suitable for other purposes like training, airplane towing, as well as for the relaxing flight on a sunny sunday.

Wild thing WT01 / WT02
Price: Not given

Ultraflight Sales
Lazair


Stall: 22 kt | 25 mph | 40 kmh
Cruise: 35 kt | 40 mph | 64 kmh
VNE: 56 kt | 65 mph | 105 kmh
Empty Weight: 95 kg | 210 lbs
MTOW Weight: 240 kg | 530 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:
Lazair, The twin engine ultralight.

The Lazair is a absolute pleasure to fly, it is perfect for that low and slow journey over the country side, it is versatile, it can be fitted with skis or floats. The aircraft is very well designed and constructed by Dale Kramer some of these ships are approaching 20 years old and they are still in great shape with a little TLC and as long as properly trained pilots fly them , they could last well into the 21 century. They also enjoy an unprecedented safety record, the few fatalities that I could find on the TSB and NTSB where attributed solely on pilot error.

Photo from: http://www.ultralightnews.com/antulbg/lazair_ultralight.htm

Text: http://persweb.direct.ca/highland/lazair/:

Lazair
Price: Not given

Ultravia Aero
Pelican Sport 450 S


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 111 kt | 127 mph | 205 kmh
VNE: 123 kt | 142 mph | 228 kmh
Empty Weight: 280 kg | 617 lbs
MTOW Weight: 523 kg | 1153 lbs
Climb Ratio: 1400 ft/min | 7,6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
The Pelican Sport 450 is a two place single-engine, high wing airplane of conventional configuration consisting of a composite fuselage and metal wings. It is equipped with a fixed tricycle landing gear.

Text and Photo: http://www.ultravia.ca

Pelican Sport 450 S
Price: Not given

Urban Air s.r.o.
UFM 13/15 Lambada


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 86 kt | 99 mph | 160 kmh
VNE: 113 kt | 130 mph | 210 kmh
Empty Weight: 280 kg | 617 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1000 ft/min | 5-7,5 m/s
Glide Ratio: 1:30
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
Ultralight motorglider.

UFM 13/15 Lambada
Price: 48000 EURO

Urban Air s.r.o.
Samba XXL


Stall: 34 kt | 39 mph | 63 kmh
Cruise: 119 kt | 137 mph | 220 kmh
VNE: 146 kt | 168 mph | 270 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 472 kg | 1041 lbs
Climb Ratio: 1400 ft/min | 7,5 m/s
Glide Ratio: 1:18
Take-off distance (50ft obstacle): 490 ft | 150 m
Landing distance (50ft obstacle): 660 ft | 200 m

Aircraft information:
Perfect plane for UL or PPL pilot training or just cruise flying.

Samba XXL
Price: 50000 EURO

US Aviation
Cumulus


Stall: 28 kt | 32 mph | 51 kmh
Cruise: 56 kt | 65 mph | 105 kmh
VNE: 78 kt | 90 mph | 145 kmh
Empty Weight: 163 kg | 360 lbs
MTOW Weight: 290 kg | 640 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 20.1
Take-off distance (50ft obstacle): 170 ft | 52 m
Landing distance (50ft obstacle): 0 ft | 0 m

Aircraft information:
The US Aviation CUMULUS... an Ultralight / Microlight Motorglider

Text and Photo From: http://members.aol.com/CumulusMan/

Note: Take-off distance not over 50ft obstacle, price is airframe only

Cumulus
Price: 7995 USD

Vol Mediterrani S.L.
VM-1 Esqual


Stall: 35 kt | 40 mph | 64 kmh
Cruise: 135 kt | 155 mph | 250 kmh
VNE: 173 kt | 199 mph | 320 kmh
Empty Weight: 270 kg | 595 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 1800 ft/min | 9 m/s
Glide Ratio: 1:19
Take-off distance (50ft obstacle): 310 ft | 95 m
Landing distance (50ft obstacle): 310 ft | 95 m

Aircraft information:
This photo was taken by Key Publishings Duncan Cybitt, during an air-to-air photo sortie for Todays Pilot magazine. The magazines editor, Dave Unwin, is seen here flying the Esqual nearest the camera plane, and a full flight test report will appear in issue 29 of Todays Pilot, on sale Feb 03. Visit the Todays Pilot web site at www.todayspilot.co.uk

http://www.esqual.com

Start and landing is not over 50 ft obstacle.

Also fitted with Jabiru Engines.

VM-1 Esqual
Price: Not given

Warner Aerocraft
Sportster


Stall: 39 kt | 45 mph | 72 kmh
Cruise: 113 kt | 130 mph | 209 kmh
VNE: 0 kt | 0 mph | 0 kmh
Empty Weight: 386 kg | 850 lbs
MTOW Weight: 680 kg | 1500 lbs
Climb Ratio: 1175 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 425 ft | 130 m
Landing distance (50ft obstacle): 400 ft | 122 m

Aircraft information:
The Sportster is a new design that we recently finished. Still the same configuration, open cockpit 2 place tandem much like the above pictured Revolution aeroplane. We've built two versions, one with both seats open, one with the front seat open or covered and the rear a removable canopy. The Sportsters have flown over 250 hours, and has completed several cross country trials, spin testing, mild aerobatic testing and is currently being flown several times a week, and used for demo rides! The Sportster is also undergoing a design stress analysis. We are very encouraged by the numbers coming back so far, we estimate stall at 45 MPH, and a 130MPH max cruise due to the more streamlined wind screens, and less wing area! The Sportster was designed to offer the taller/wider pilots an alternative. It keeps the same look as all the Warner line of aerocraft but the fuselage is stretched and widened to allow 6'5" tall pilots to fly in comfort. Of course being open cockpit, tall doesn't seem to be a problem from first glance (no top) but the cockpit of the prior airplanes was limited by leg room. We typically attend the Lakeland Sun N Fun and Oshkosh airshows. The Sportster flying quality report can be found in the in the August 2000 Sport Aviation magazine ( a big thank you to EAA) it was a big hit and are currently taking orders for the kit. The Sportster is currently planned for kit only sales and we do not currently intend to offer a "plans only" option for the aerocraft.

Text and Photo from: http://www.warnerair.com/

Notes: Aircraft sold as kit and take-off and landing distance not over 50ft obstacle.

Sportster
Price: 16495 USD

Weedhopper
Model 40


Stall: 17 kt | 20 mph | 32 kmh
Cruise: 48 kt | 55 mph | 89 kmh
VNE: 56 kt | 65 mph | 105 kmh
Empty Weight: 113 kg | 250 lbs
MTOW Weight: 249 kg | 550 lbs
Climb Ratio: 1000 ft/min | 5 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 100 ft | 30 m
Landing distance (50ft obstacle): 100 ft | 30 m

Aircraft information:
Photo from http://www.weedhopperusa.net/

Model 40
Price: 7995 USD

WZL nr 3 Deblin, Poland
DEKO-9


Stall: 49 kt | 56 mph | 90 kmh
Cruise: 103 kt | 118 mph | 190 kmh
VNE: 189 kt | 217 mph | 350 kmh
Empty Weight: 590 kg | 1301 lbs
MTOW Weight: 800 kg | 1764 lbs
Climb Ratio: 1400 ft/min | 7 m/s
Glide Ratio: 7
Take-off distance (50ft obstacle): 390 ft | 120 m
Landing distance (50ft obstacle): 390 ft | 120 m

Aircraft information:
DEKO-9 was designed by Polish world renowned aeronautical engineers: Marek Debski, Krzysztof Kotlinski, Daniel Debski, Marian Jakoniuk. Design begun in 1995, prototype exhibited at ILA 1998 and ILA 2000 Berlin, first flight September 2000. Design Features: Fully aerobatic, classic biplane. Structure: Aluminum tube fuselage with composite joints (Polish Patent) and with Ceconite covering. Power Plant: PZL Franklin 6A-350C1R (205 hp) with MT-Propeller MTV-9-D-C/C188-18a three-blade, variable-pitch propeller. More info: http://www.dkd1970.webpark.pl/

DEKO-9
Price: Not given

WZL nr 3 Deblin, Poland
DEKO-6 Whisper


Stall: 35 kt | 40 mph | 65 kmh
Cruise: 76 kt | 87 mph | 140 kmh
VNE: 103 kt | 118 mph | 190 kmh
Empty Weight: 290 kg | 639 lbs
MTOW Weight: 490 kg | 1080 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: 8
Take-off distance (50ft obstacle): 230 ft | 70 m
Landing distance (50ft obstacle): 260 ft | 80 m

Aircraft information:
DEKO-6 Whisper was designed by Polish aeronautical engineers: Marek Debski, Krzysztof Kotlinski, Daniel Debski, Marian Jakoniuk. Type: Side-by-side ultra and very light training and observation aircraft. Exhibited incomplete at Aero’99, ILA 2000, and Aero’2001. Design Features: Pod-and-boom fuselage. Wings braced by V-type struts. Two-section Junkers-type flaps and separate ailerons. Structure: Principally riveted aluminium with composite joints (Polish Patent). Ceconite covering and glass fibre pod and control surfaces. Power Plant: One Hirth F30 (79 hp) four-cylinder piston engine. Propeller Junkers three-blade, carbon fibre, ground-adjustable pitch propeller. System: Ballistic parachute recovery system More info: http://www.dkd1970.webpark.pl/ , Jane’s All the World’s Aircraft 2003-2004 Contact: dedal@ilot.edu.pl

DEKO-6 Whisper
Price: Not given

X-Air
X-Air


Stall: 26 kt | 30 mph | 48 kmh
Cruise: 61 kt | 70 mph | 113 kmh
VNE: 83 kt | 95 mph | 153 kmh
Empty Weight: 243 kg | 536 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 900 ft/min | 5 m/s
Glide Ratio: 1:7
Take-off distance (50ft obstacle): 880 ft | 269 m
Landing distance (50ft obstacle): 750 ft | 230 m

Aircraft information:
X-air Kit price Only £5900.00 + delivery & vat The only extra cost will be the Engine & Instruments of your choice. The X-air comes in a range of 15 different colour combinations. Image from and more info at: http://www.esatclear.ie/~xair/index.htm

X-Air
Price: Not given

X-Air
Hanuman


Stall: 29 kt | 33 mph | 53 kmh
Cruise: 76 kt | 87 mph | 140 kmh
VNE: 105 kt | 121 mph | 195 kmh
Empty Weight: 263 kg | 580 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: 900 ft/min | 4.8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 360 ft | 110 m
Landing distance (50ft obstacle): 720 ft | 220 m

Aircraft information:
Text and Photo from: http://www.randkar.fr/ X-AIR HANUMAN is the new aircraft from RANDKAR-RAJHAMSA. It's a 3 axis ultralight available in kit or ready to fly in a very large range of colors.

Hanuman
Price: Not given

Zlín Aviation s.r.o.
Savage


Stall: 31 kt | 36 mph | 58 kmh
Cruise: 92 kt | 106 mph | 170 kmh
VNE: 111 kt | 127 mph | 205 kmh
Empty Weight: 288 kg | 635 lbs
MTOW Weight: 560 kg | 1235 lbs
Climb Ratio: 800 ft/min | 4,8 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 520 ft | 160 m

Aircraft information:
Data from www.aerosavage.com Photo from www.ulm.it The Savage is a single-engine, high-wing, two-seater tandem microlight aircraft of classic design. It is built in the Czech Republic in full compliance with the aeronautical regulations in force in that country.

Savage
Price: Not given

Light Aircraft Database - www.pilotmix.com