Ultralight / ULM and LSA Aircraft for Sport Pilots
This is a collection of the aircraft at pilotmix.com that are either classified as LSA or ULM / Ultralights.
Some of these aircraft are also classified as homebuilts since they are sold as kits and you have to assemble them yourself.
So have you ever dreamed about owning your own airplane? Browse these aircraft and follow the links to read more about them.
[sort by aircraft model]
Stall: 34 kt | 39 mph | 63 kmh
Cruise: 94 kt | 109 mph | 175 kmh
VNE: 117 kt | 134 mph | 216 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 450 kg | 992 lbs
Climb Ratio: - ft/min | 0 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 740 ft | 225 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: The
3Xtrim is a single-engine, two-seater monoplane with braced high wing,
conventional controls and fixed three-wheel landing gear. The
front-mounted engine is coupled to a two-blade or three-blade
(depending on version) adjustable pulling propeller. A spacious, heated
and ventilated cockpit with seats in one row and a large baggage
compartment make the airplane comfortable, silent and well furbished.
Access is easy through doors on each side opening upwards and supported
in this position by gas springs. Fixed three-wheel landing gear with
castoring front wheel, composite main spring and hydraulic disc brakes,
ensures safe take-off and landing on all types of airport surfaces,
grass included. The Ballistic Rescue System (BRS5) provides protection
for the passengers and aircraft at altitudes above 30 m and speeds up
to 235 kmph (145 mph). The aircraft structure is fabricated from
composites based on epoxy resin with glass and carbon fibre. This
totally composite structure reduces necessary maintenance work to
pre-flight inspection and cleaning. The aircraft fully complies with
the JAR-VLA requirements and has a Type Certificate of Very Light
Airplane. Excellent flight characteristics make this aircraft a perfect
choice for primary schooling, training, travelling, and recreation. The
aircraft is just as suitable for patrol flights and aerial photography.
Flying is precise, easy, safe, and pleasant. Thanks to the incorporated
technical solutions, components and materials, operational costs are
low and comparable with a medium-class passenger car. A three-years
manufacturer\'s warranty is standard.
The aircraft is manufactured in three versions: * ULA - \"Ultra Light
Aircraft\" * AULA - \"Advanced Ultra Light Aircraft\" * VLA - \"Very
Light Aircraft\" Text and photo from: www.3xtrim.pl |
|
Price: Not given
|
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/
|
|
Price: Not given
|
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/
|
|
Price: 65000 EURO
|
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/
|
|
Price: 18950 USD
|
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/
|
|
Price: 20950 USD
|
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
|
|
Price: Not given
|
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: -
|
|
Price: Not given
|
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: -
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 35995 USD
|
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.
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 42000 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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. |
|
Price: 30000 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: 39500 EURO
|
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. |
|
Price: 18000 USD
|
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
|
|
Price: 60000 EURO
|
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. |
|
Price: Not given
|
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/
|
|
Price: Not given
|
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 |
|
Price: Not given
|
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/ |
|
Price: Not given
|
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
|
|
Price: Not given
|
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!
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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
|
|
Price: 3000 USD
|
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 |
|
Price: 20 EURO
|
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 |
|
Price: 17995 USD
|
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 |
|
Price: 19995 USD
|
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 |
|
Price: 20995 USD
|
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 |
|
Price: 27500 USD
|
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 |
|
Price: 15950 USD
|
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 |
|
Price: 13150 USD
|
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 |
|
Price: Not given
|
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/
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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: -
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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 |
|
Price: 66000 EURO
|
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 |
|
Price: 42500 EURO
|
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
|
|
Price: 52000 USD
|
Stall: 23 kt | 27 mph | 43 kmh
Cruise: 48 kt | 55 mph | 89 kmh
VNE: 55 kt | 63 mph | 101 kmh
Empty Weight: 104 kg | 230 lbs
MTOW Weight: 209 kg | 460 lbs
Climb Ratio: 500 ft/min | 3 m/s
Glide Ratio: N/A
Take-off distance (50ft obstacle): 300 ft | 91 m
Landing distance (50ft obstacle): 250 ft | 76 m
Aircraft information: July
2003 : The Eureka has been withdrawn from the market due to lack of
resources. We will continue to answer all e-mail ! wstark@nucleus.com
The website will remain for informational purposes only.
http://www.nucleus.com/~eureka/
The Eureka was developed after recognizing that the current market does
not offer an affordable Ultralight that is also easy to build.
Eureka is a machine that can be put into the air, ready-to-fly, for
about $8000 |
|
Price: 8000 USD
|
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
|
|
Price: Not given
|
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/
|
|
Price: 11700 USD
|
Stall: 33 kt | 38 mph | 61 kmh
Cruise: 127 kt | 146 mph | 235 kmh
VNE: 157 kt | 180 mph | 290 kmh
Empty Weight: 235 kg | 518 lbs
MTOW Weight: 470 kg | 1036 lbs
Climb Ratio: 1259 ft/min | 6 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 620 ft | 190 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Light Two-seater Motorgliders Family
- for all reasons and seasons
- soaring, towing, cruising,training
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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.
|
|
Price: Not given
|
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).
|
|
Price: Not given
|
Stall: 34 kt | 39 mph | 63 kmh
Cruise: 103 kt | 118 mph | 190 kmh
VNE: 139 kt | 160 mph | 258 kmh
Empty Weight: 0 kg | 0 lbs
MTOW Weight: 0 kg | 0 lbs
Climb Ratio: 800 ft/min | 4 m/s
Glide Ratio: -
Take-off distance (50ft obstacle): 0 ft | 0 m
Landing distance (50ft obstacle): 0 ft | 0 m
Aircraft information: Ultralight Aircraft with retractable gear - options available -
ready to fly starting of 66.000 €
visit
www.capco-aviation.be
|
|
Price: 66000 EURO
|
Stall: 35 kt | 40 mph | 65 kmh
Cruise: 130 kt | 150 mph | 241 kmh
VNE: 143 kt | 165 mph | 265 kmh
Empty Weight: 265 kg | 584 lbs
MTOW Weight: 550 kg | 1213 lbs
Climb Ratio: 1700 ft/min | 9 m/s
Glide Ratio: 1:17
Take-off distance (50ft obstacle): 660 ft | 200 m
Landing distance (50ft obstacle): 660 ft | 200 m
Aircraft information: This
aerodynamic, cantilevered, low wing sport pilot aircraft of mixed
construction can transport two people over 800 statute miles at a
maximum cruising speed of 155 mph. And it all begins with a quick 200
to 400 foot ground roll on a grass or concrete strip. Before you know
it, you're in the air, rapidly accelerating toward a maximum climb rate
of nearly 1,700 feet per minute!
But that's not all because, with the history behind the ATEC Zephyr, you have peace of mind.
Developed in collaboration with renowned Czech aircraft designer,
Oldrich Olsansky, the ATEC Zephyr Sport Pilot airplane has an
impeccable safety record since its debut over six years ago. With over
110 units plying the skies of Australia, Europe and North America, the
plane is thoroughly proven and exceptional from a reliability and
economic standpoint.
What's more, buyers have two paths to choose from when it comes to
buying one. Sport Pilot, Amateur-built (Experimental in the U.S.) or
Ultralight (Canada only; Advanced Ultralight pending). By opting for
the first category, operators can enjoy all of the benefits of a
fully-certified aircraft minus outrageous acquisition, operating and
maintenance costs. Moreover, they can even train student pilots in a
flying club environment. For those who no longer qualify for the
standard aviation medical, the Ultralight and Sport Pilot categories
less restrictive requirements may be the answer. Either way, one
thing's sure. With an ATEC Zephyr, you no longer have to sacrifice
performance and flexibility for affordability.
The MTOW is 472.5 kg in the European ultralight version and in US the
LSA version of the Zephyr allows 550 kg. The LSA Zephyr is called
Zephyr 2550.
Text from: http://www.atecaviation.com/ |
|
Price: 44000 EURO
|
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/
|
|
Price: Not given
|
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: -
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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
|
|
Price: 46000 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 18000 USD
|
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: -
|
|
Price: 6000 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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 |
|
Price: 69 USD
|
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
|
|
Price: 20000 USD
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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
|
|
Price: Not given
|
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)
|
|
Price: 40000 EURO
|
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: -
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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.” |
|
Price: Not given
|
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)
|
|
Price: 64000 EURO
|
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 |
|
Price: Not given
|
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
|
|
Price: 84000 EURO
|
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 |
|
Price: 100 EURO
|
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/
|
|
Price: Not given
|
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.
|
|
Price: 13499 EURO
|
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.
|
|
Price: Not given
|
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
|
|
Price: 44000 EURO
|
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. |
|
Price: Not given
|
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. |
|
Price: Not given
|
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.
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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
|
|
Price: 33804 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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.
|
|
Price: 15000 EURO
|
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
|
|
Price: 35000 EURO
|
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.
|
|
Price: Not given
|
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 |
|
Price: 41000 EURO
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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
|
|
Price: 50000 EURO
|
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. |
|
Price: 6200 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 12650 USD
|
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
|
|
Price: 8750 USD
|
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
|
|
Price: 15500 USD
|
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/
|
|
Price: 14300 USD
|
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
|
|
Price: 55862 EURO
|
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/
|
|
Price: 60000 EURO
|
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/
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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. |
|
Price: 24950 EURO
|
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 ... |
|
Price: Not given
|
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! |
|
Price: Not given
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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 |
|
Price: Not given
|
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 |
|
Price: Not given
|
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
|
|
Price: 18320 USD
|
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
|
|
Price: 12410 USD
|
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/ |
|
Price: Not given
|
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. |
|
Price: Not given
|
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/
|
|
Price: Not given
|
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 |
|
Price: 30 USD
|
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. |
|
Price: 30000 USD
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 33000 EURO
|
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!
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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 |
|
Price: Not given
|
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/
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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.
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 9000 EURO
|
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 |
|
Price: 36900 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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.
|
|
Price: 15000 USD
|
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/
|
|
Price: 12000 EURO
|
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.
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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.
|
|
Price: 14 USD
|
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
|
|
Price: 17000 USD
|
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. |
|
Price: Not given
|
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 |
|
Price: Not given
|
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 |
|
Price: Not given
|
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
|
|
Price: 60000 EURO
|
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/
|
|
Price: Not given
|
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.
|
|
Price: 34500 USD
|
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.
|
|
Price: 19895 USD
|
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/
|
|
Price: Not given
|
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. |
|
Price: 27150 EURO
|
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 |
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 49000 EURO
|
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.
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 46900 EURO
|
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
|
|
Price: 57900 EURO
|
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
|
|
Price: 57900 EURO
|
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
|
|
Price: 70000 EURO
|
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/
|
|
Price: Not given
|
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 |
|
Price: Not given
|
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: -
|
|
Price: Not given
|
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: -
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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
|
|
Price: 16 USD
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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 |
|
Price: Not given
|
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
|
|
Price: 14700 USD
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 92800 EURO
|
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
|
|
Price: 78800 EURO
|
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
|
|
Price: 35000 EURO
|
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.
|
|
Price: 15000 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 85000 EURO
|
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.
|
|
Price: 34000 USD
|
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
|
|
Price: 50170 EURO
|
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
|
|
Price: 40000 EURO
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 95000 USD
|
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/
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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.
|
|
Price: 11073 USD
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 45000 EURO
|
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: -
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: 15995 USD
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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: -
|
|
Price: Not given
|
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: -
|
|
Price: Not given
|
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/
|
|
Price: 22900 EURO
|
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/
|
|
Price: Not given
|
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
|
|
Price: 18700 USD
|
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
|
|
Price: 68000 USD
|
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
|
|
Price: 9000 USD
|
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
|
|
Price: 24900 USD
|
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.
|
|
Price: 37500 USD
|
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
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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/
|
|
Price: Not given
|
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. |
|
Price: Not given
|
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. |
|
Price: 56000 EURO
|
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. |
|
Price: Not given
|
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)! |
|
Price: 42500 EURO
|
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
|
|
Price: 47000 EURO
|
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: -
|
|
Price: 15000 EURO
|
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
|
|
Price: 18950 USD
|
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. |
|
Price: Not given
|
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/:
|
|
Price: Not given
|
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
|
|
Price: Not given
|
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.
|
|
Price: 48000 EURO
|
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.
|
|
Price: 50000 EURO
|
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
|
|
Price: 7995 USD
|
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.
|
|
Price: Not given
|
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.
|
|
Price: 16495 USD
|
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/
|
|
Price: 7995 USD
|
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/ |
|
Price: Not given
|
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 |
|
Price: Not given
|
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
|
|
Price: Not given
|
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.
|
|
Price: Not given
|
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. |
|
Price: Not given
|
|
|