ULL Classic - old.laacr.czold.laacr.cz/pictures/AERO2011/02_aircraft.pdf · the Rotax 912 UL / ULS...

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ULL ClassicClassic - A two-seat side by side high wing braced composite monoplane for both ULL and LSA category. Powered by the Rotax 912 UL / ULS touring on ground adjustable or constant speed propeller.

Span 9,1 m,lenght 6,3 m,wing area 9,9 m2

empty weight 285 kgcruising speed 180 -220 km/h

Aerospool CZ, s.r.o.Hlavní 439687 25 HlukCzech Republicwww.aerospool.cze-mail: [email protected]

SkylaneA two-seat side-by-side braced high-wing ultralight monoplane of mixed, mainly composite structure. Fixed tricycle under-carriage. The aircraft is designed for wide range of usage – from trainer to long distance tourer. Main features are: roomy luggage compartment, high useful load, high cruising speed, long flying range. It is powered by Rotax 912. (So far 48 machines built.) Span: 8,95 m, length: 6,65 m,wing area: 10,57 m2,empty weight: 248 kg,cruising speed: 140 - 210 km/h.

AirLony,Nové Náměstí 702, 411 08 Štětí,Czech Republicwww.airlony.cze−mail: [email protected]

MH−46 EclipseUltralight two−seat braced high−wing monoplane. It is very controllable and features a spacious cockpit for two side−by−side pilots. The tricycle undercar-riage is fixed, power is provided by Rotax 912S engine, turning a three−bladed variable−pitch propeller. (5 aircraft pro-duced so far.)

Span 9,80 m, length 6,75 m,wing area 11,30 m2,cruising speed 190 − 250 km/h.

AeroSette, spol. s r.o.,Nádražní 20,463 31 Chrastava, Czech Republicwww.aerosette.eue−mail: [email protected]

UL-LSA AIRCRAFT

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Atec 321 FaetaA two−seat side−by−side low−wing ultra light airplane of mixed (composite and wood) structure. Fixed tricycle undercarriage. Powered by Rotax 912UL or ULS, with fixed or variabl−pitch propellers. Aeroplane is also officially certified as a towing plane. The Atec 322 Faeta is the LSA version. (So far 70 machines built.)

Span 9,60 m, length 6,20 m,wing area 10,10 m2,empty weight 268 kg,max. level speed VH 250 km/h.

Atec, v.o.s.,Opolanská 350, 289 07 Libice nad Cidlinou,Czech Republicwww.atecaircraft.eue−mail: [email protected]

Atec 212 SoloA single−seat ultralight airplane of com-posite structure. Fixed tailwheel undercar-riage. Stressed for +6/−3 g. Powered by Rotax 582UL DCDI or 912UL. (So far 7 machines built.)



HighlanderA tandem two-seat ultralight biplane of mixed, mainly composite structure. Fixed tailwheel undercarriage. Highlander is designed for leisure and joyful flying with accent on safety. Aircraft is powered by Rotax 912 ULS and has increased G-limits up to +6/-4g.

Span: 7,3 m, length: 6,05m,wing area: 14,3 m2,empty weight: 230kg,cruising speed: 100 – 140 km/h.

AirLony,Nové Náměstí 702, 411 08 Štětí,Czech Republicwww.airlony.cze−mail: [email protected]

CZECH AVIATION 2011CZECH AVIATION 2011

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NG 5UL, ELSA, LSA, RG – all metal two seat-er powered by Rotax 912 ULS, Jabiru 2200/3300 engines. Ultralight aeroplane NG 5 is intended for flight training in flight schools, gliders towing and recreational flying. Thanks to large cockipt and good ergonomy NG is an ideal vehicle for long cross country flights. One prototype has been builded so far.

Span 8,13 m, length 6,45 m,wing area UL/LSA,RG 10/11,75 m2,empty weight UL/LSA,RG 290/320 kg,cruising speed UL/LSA,RG 214/240 km/h.

BRM Aero s.r.o.Václava Kulíška 1224686 05 Uherské HradištěCzech [email protected]

Atec 122 ZephyrA two−seat side−by−side low−wing ultra light airplane of mixed (composite and wood) structure. Fixed tricycle undercar-riage. Powered by Rotax 912UL or ULS, with fixed or variable−pitch propellers. (215 units built so far.)



VL−3 SprintA two−seat side−by−side low−wing all−composite monoplane approved for both ultralight and LSA category. Available with retractable or fixed landing gear. Powered with Rotax 912ULS with fixed or variable−pitch propellers. VL−3 holds 3 world speed records in RAL2 category. (almost 100 aircraft produced so far.)

Span 8,44 m, length 6,20 m,wing area 9,80 m2,empty weight 280−305 kg,max. level speed VH 280 km/h.

Vanessa air, s.r.o.,Toulovcovo nám. 1163,570 01 Litomyšl,Czech Republicwww. vanessaair.cz e− mail: [email protected]

Design: Manufacturer:

Aveko Aircraft, a.s.,Lipová 22,602 00 Brno,Czech Republicwww.VL−3.come−mail: VL−[email protected]

CZECH AVIATION 2011UL-LSA AIRCRAFT

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AltoAn all−metal cantilever low−wing ultralight monoplane, seating two side−by−side. It can be bought in the Alto TW version with a tailwheel and in the Alto TG version with a tricycle undercarriage. Powered by Rotax 912 or Jabiru (60kW/80hp to 90kW/120hp range). Also available as a homebuilding kit in various states of pre−assembly. (31 aircraft have been built so far).

Span 8,20 m, length 6,25 m,wing area 10,50 m2,empty weight 285 kg,cruising speed 195 km/h.

Direct Fly, s.r.o., Cihelní 573, 687 25 Hluk,Czech Republicwww.directfly.cz, www.flyshop.cze−mail: [email protected]

PS-10 TourerAll-metal, two-seater, high-wing LSA air-plane, intended for training, tourist and patrol flights. The airframe design concept is adjusted to this purpose – self-sup-porting wing and the cockpit situated on the wing leading edge level to provide en excellent views for the crew. Powered with Rotax 912 ULS engine and a three-blade fixed propeller.One prototype of this model was built.Span 9,5 m, length 7,1 m,wing area 11,5 m2,empty weight 340 kg,cruising speed 210 km/h.

Czech Sport Aircraft a.s.Na Záhonech 1177/212Kunovice 686 04,Czech RepublicPhone: + 420 576 514 032Fax: + 420 576 519 394e-mail: [email protected]

PS-28 CruiserAll-metal, two-seater, low-wing LSA air-plane, intended for training, tourist flying and towing of gliders.The aircraft is normally equipped with Rotax 912 ULS engine and a three-blade fixed propeller. Nevertheless, a variable pitch propeller installation is possible as well.The total number of aircraft produced is 426.

Span 8,53 m, length 6,16 m,wing area 12,3 m2.empty weight 340 kg,cruising speed 200 km/h.

Czech Sport Aircraft a.s.Na Záhonech 1177/212Kunovice 686 04, Czech RepublicPhone: + 420 576 514 032Fax: + 420 576 519 394e-mail: [email protected]


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UFM−13 LambadaA side−by−side two−seat, mid−wing ultra-light of composite structure. Fixed tri-cycle or tailwheel undercarriage. Powered by Rotax 912UL, ULS or Jabiru 2200 engines, with fixed or variable−pitch pro-peller. The wing may be fitted with wingtip extensions, increasing the span to 15 m. (So far 135 aircraft in the UFM−11 −13 ver-sions have been produced.)

Span 13,00 m, length 6,60 m,wing area 12,60 m2,empty weight 265 − 280 kg,cruising speed 150 km/h.

DV−1 SkylarkA two−seat, side−by−side, all−metal low−wing ultralight. Fixed tricycle undercarriage. Powered by Rotax 912ULS, eventually BMW or Alpha Prag engines. Propellers are fixed or variable−pitch. There is also an LSA version. (169 machines have been built during 10 years of production.)

Span 8,13 m, length 6,62 m, wing area 9,84 m2, empty weight 285 kg,cruising speed 215 km/h.

Dova Aircraft, s.r.o.,Kirilovova 115, 739 21 Paskov,Czech Republicwww.dovaaircraft.cze−mail: [email protected]

ArgoClassical all-metal high-wing Ultralight or LSA aircraft, with side-by-side seats, pow-ered by Rotax 912 UL/ULS.Designed to be ideal for training and also for cross-country flying.

Span 9,0 m, length 5,58 m,wing area 9,9 m2,empty weight UL / LSA, ELSA 282 / 297 kg,cruising speed 200 km/h.

Direct Fly, s.r.o., Cihelní 573, 687 25 Hluk,Czech Republicwww.directfly.cz, www.flyshop.cze−mail: [email protected]

Production division:

Distar − Air,U Letiště 1381,562 01 Ústí nad OrlicíCzech Republic

Company headquarters:

Distar CZ, a.s.,1. máje 228,504 01 Nový Bydžov,Czech Republice−mail: [email protected]−mail: [email protected]


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SR−01 MagicTandem two−seat low−wing all−metal monoplane with tricycle fixed undercar-riage. Powered by Rotax 912ULS, turn-ing a Woodcomp three−blade composite propeller. The machine is designed for the UL and LSA category. 2 prototypes has been builded so far.

Span 9,44 m, length 6,96 m,wing area 11,73 m2,max. cruising speed 220 km/h.

Eurodisplay, s.r.o.,Průmyslová zóna Kozomín, 278 01 Kralupy nad Vltavou,Czech Republicwww.aeromagic.cze−mail: [email protected]

Samba XXLA low−wing, composite side−by−side two−seat ultralight monoplane. Fixed tri-cycle undercarriage. Powered by Rotax 912UL or ULS engines, with fixed or variable−pitch propeller. (93 aircraft have been built so far).


EuroStar SL / SLW A side−by−side two−seat cantilever low−wing advanced ultralight aircraft of all metal structure. Fixed tricycle under-carriage. Powered by Rotax 912UL or ULS engines, with fixed of variable pitch propeller. EuroStar SLW version uses LSA airframe with a wet wing and range 1300 km.

Span 8,10 m, length 5,98 m,wing area 9,84 m2,weight 264 kg,cruising speed 210 − 245 km/h.

Evektor−Aerotechnik, a.s., Letecká 1384, 686 04 Kunovice, Czech Republic www.evektoraircraft.come−mail: [email protected]

Production division:

Distar − Air,U Letiště 1381,562 01 Ústí nad OrlicíCzech Republic

Company headquarters:

Distar CZ, a.s.,1. máje 228,504 01 Nový Bydžov,Czech Republice−mail: [email protected]−mail: [email protected]


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SportStar MAX An all metal side−by−side two−seat S−LSA aircraft − the very first aircraft in the world approved by the FAA in the US S−LSA cat-egory. Powered by Rotax 912ULS engine, with fixed or variable pich propeller. Fixed tricycle undercarriage. Altogether over 1000 aircraft of the EuroStar/SportStar line have been built.



SportStar RTCAn all metal side−by−side two−seat train-ing airplane designed according to new EASA CS-LSA regulation using airframe from EASA JAR-VLA certified trainer called Harmony. Powered by Rotax 912S engine, with fixed or variable pich propeller. Fixed tricycle undercarriage.



Harmony / Harmony LSAA side−by−side two−seat cantilever low-wing advanced UL / LSA aircraft of all metal structure. Fixed tricycle undercar-riage. Powered by Rotax 912UL or ULS engines, with fixed of variable pitch pro-peller. The Harmony has curved wing, 120 l wing tanks providing 1300 km range and outstanding cockpit spaciousness.




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FM−250 Vampire II FM−250 Vampire is an all composite low wing ultralight side−by−side two−seater. It is powered by Rotax 912 and has use-ful load of 190 kg. It is capable of towing gli−ders up to 700 kg MTOM. Used as a training aircraft in flight schools as well as a long range UL tourer.

Span 7,80 m, length 6,26 m,empty weight 272,5 kg,cruising speed 180 − 230 km/h.

Flying Machines, s.r.o.,Rasošky 132,55221 Rasošky,Czech Republicwww.flyingmachines.cze−mail: [email protected]

Evolution E80 / E100A side−by−side two−seat, cantilever shoulder−wing monoplane of composite structure. Wing with slotted flaps, fixed or retractable tricycle undercarriage. Powered by Rotax 912UL (ULS), turning a ground−adjustable DUC, or variable−pitch Woodcomp SR 3000/2W propeller.

Span 9,00 m, length 6,65 m,wing area 10,76 m2,weight 305 kg,cruising speed 243 km/h.

Fascination a.s.Příkop 6/838 602 00Brno www.fascination.aero e-mail:[email protected]

Fascination F80 / F100A side−by−side two−seat, cantilever low−wing monoplane of all−composite structure. Wing with slotted flaps, fixed or retractable tricycle undercarriage. Powered by Rotax 912UL (ULS), turning a ground−adjustable DUC, or variable−pitch Woodcomp SR 3000/2W propeller.

Span 9,00 m, length 6,65 m,wing area 10,76 m2,weight 294 kg,cruising speed 247 km/h.

Fascination a.s.Příkop 6/838 602 00Brno www.fascination.aero e-mail:[email protected]


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ZJ−VieraThe true motorbike of the sky. ZJ−Viera is an extremely lightweight single−seater, designed by Marek Ivanov. Of mainly composite structure, its wing is partly co−vered in Ceconite fabric. Powered by a single−cylinder Flyengine F200 two−stroke of 19 kW/26 hp.


Ivanov Aircraft s.r.o.Tr. E. Beneše 156150012 Hradec KraloveCzech Republicwww.IvanovAero.cze−mail: [email protected]

Skyleader 100The Skyleader 100 is an all metal one-seat, low wing, ultralight aircraft with a rectan-gular or trapezoidal wing. The aircraft has a conventional “taildragger” landing gear with a fixed gear option only. The aircraft are designated mainly for recreational flying. Engine type: Rotax 503UL. One prototype has been built so far.


Jihlavan Airplanes, s.r.o.Znojemská 826/64586 01 JihlavaCzech Republice-mail: [email protected]

FM−301 StreamFM-301 Stream is an all composite two seat-er microlight trike of frameless load bearing construction. The aerodynamic shape of the machine makes it quite easy and com-fortable to handle both on ground as well as in air. The main landing gear is installed at the back of the trike which makes it easy to install, inspect and maintain. A unique feature of the FM301 is its spacious instru-ment panel, which offers plenty of space for installation of more than just the basic flight and engine instruments.Weight ready to fly (Rotax 912, Rescue system, Wing CZ 15,4) 223 kg

Flying Machines, s.r.o.,Rasošky 132,55221 Rasošky,Czech Republicwww.flyingmachines.cze−mail: [email protected]


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Skyleader GP ONEThe Skyleader GP ONE is carbon-com-posite two-seat, high wing ultralight air-craft with a monocoque construction. The aircraft has a tricycle towed landing gear with a steerable nose wheel and fixed gear. This aircraft is designated mainly for pilot training and low-cost flying. One prototype has been built so far.Engine type: Rotax 912 UL.


Jihlavan Airplanes, s.r.o.Znojemská 826/64, 586 01 Jihlava,Czech Republicwww.skyleader.aero

Skyleader 600The Skyleader 600 is an all metal two-seat, low wing, constructed aircraft with a trapezoidal wing. The aircraft has a tri-cycle towed landing gear with a steerable nose wheel and either retractable or fixed gear options. The aircraft are designated mainly for recreational flying, pilot train-ing and special operations. Engine type: Rotax 912 UL, ULS or 914UL. (3 aircraft have been built so far)

Span 9,90 m, length 7,0 m,wing area 11,85 m2,empty weight 313 kg, MTOM 600 kg,cruising speed 220 km/h.


Skyleader 200 / 500The Skyleader 200 is an all metal two-seat, low wing, UL/LSA aircraft with a tra-pezoidal wing. The aircraft has a tricycle towed landing gear with a steerable nose wheel and either retractable or fixed gear options. The aircraft are designated main-ly for recreational flying, pilot training and special operations. Engine type: Rotax 912 UL, ULS or 914UL. (165/43 aircraft have been built so far.)

Span 9,90 m, length 7,0 m,wing area 11,85 m2,empty weight 298/313 kg, MTOM 450/580 kgcruising speed 215 km/h.



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JoraA composite−structure, braced high−wing side−by−side two−seat ultralight. Fixed tricycle undercarriage. Powered by a choice of engines − Jabiru 2200, Rotax 912UL or Rotax 582. The propel-ler is a two−bladed, ground−adjustable Wood−comp. (133 aircraft have been built, including the kits.)

Span 9,80 m, length 6,05 m,wing area 11,40 m2,weight 262 − 275 kg,max. level speed VH 186 km/h.

Jora, spol. s r.o.565 42 Vraclav,Czech Republic, www.jora.cze−mail: [email protected]

SD-1 MinisportA single seat cantilever low-wing UL/LSA aircraft of mixed wood/composite con-struction with fixed undercariage in tail-dragger or tricycle configuration. It could be powered by engines in the range of 23-50 HP. Also suitable for amateur con-struction. (30 kit-built aircraft have been produced so far.)

Span 6 m, lenght 4,3 mWing area 6 m2

empty weight 120 kggross weight 240 kgmax. speed in horizontal flight 190 km/h.

Spacek s.r.o. Lesní 25695 01 HodonínCzech republicwww.sdplanes.come-mail:[email protected]

M−2 ScoutA side-by-side two seater low wing aircraft of classic shapes and “retro” look avail-able in UL and LSA versions. Powered by Rotax 912 with fixed or variable pitch pro-peller. Fixed tricycle undercariage, nose-wheel steerable. (3 aircraft have been built so far).

Span 9,40 m, length 6,75 m,wing area 12,90 m2,empty weight 295 kg,cruising speed 180 − 220 km/h.

Kubíček Aircraft, s.r.o.Jarní 2b614 00 BrnoCzech Republicwww.kubicekaircraft.cze-mail: [email protected]


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SharkA tandem two-seat high performance ultra-light/LSA/ELA low wing with all-composite, mostly carbon airframe. Retractable under-carriage for MTOW 472.5kg UL and 600 kg experimental versions, fixed u/c and LSA/ELA under development. Powered by Rotax 912 ULS, variable pitch propeller. Two pro-totypes flying, initial serial production in progress.

Span 7,9 m, length 6,7 m,wing area 9,5 m2, empty weight 295 kg (incl. BRS), max. cruising speed VH 295 km/h, flight range 1600 km

Shark.Aero CZ s.r.o. Mladá 835687 25 HlukCzech Republicwww.shark.aeroe-mail: [email protected]

TL-3000 SiriusA side-by-side two seat light sport high wing carbon composite aircraft with fixed tricycle undercarrieage. Powered by the Rotax 912UL, 912ULS turning a ground adjustable three-bladed propeller. TL 3000 Sirius – the perfect partner for fun flying without limits.

Span 9.40 m, length 6.75 m, wing area 11.15 m2, empty weight 297 kg, max. speed in horizontall flight 230 km/h.

TL-ultralight s.r.o.Letiště − budova č. 84503 41 Hradec Králové, Czech Republicwww.tl-ultralight.cze-mail: [email protected]

TL-2000 Sting S4New innovated version of successful model Sting has been aerodynamically improved with new clean lines not only improving performance but also appearance and the elegant new look is certainly a class leader. The Sting S4 is a two seater low-wing air-craft made from carbon fiber. Powered by Rotax 912UL or 912ULS, turning a ground-adjustable or variable pitch three-bladed propeller. The newly designed Sting S4 grabs you and doesn´t let you go.

Span 9.11 m, length 6.2 m, wing area 10.52 m2, empty weight 297 kg, max. speed in horizontal flight 270 km/h.



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Tulák DandyA two−seat side−by−side high−wing braced ultralight monoplane of classic design. All−wood flapped wing is mated to a welded steel tube truss fuselage and empennage. Fixed tailwheel undercar-riage. Powered by Rotax 503 or 912 and similar powerplants. (So far 68 aircraft flown.)

Span 9,80 m, length 5,60 m,wing area 10,80 m2,empty weight 255 kg,cruising speed 100 − 140 km/h.

Tomáš Podešva, výroba a opravy UL letadelÚjezd u Uničova 87, 783 96,Czech Republicwww.podesva−air.come−mail:[email protected]

TL-2000 StingA side-by-side two-seat cantilever low-wing light sport aircraft of composite con-struction with fixed or retractable tricycle undercarriage. Powered by Rotax 912UL or 912ULS, turning a ground-adjustable or variable-pitch three-bladed propeller. (More than 500 Stings have been manu-factured).

Span 8.44 m, length 6.19 m, wing area 9.81 m2, empty weight 297 kg, max. speed in horizontal flight 270 km/h.


Viper SD-4Viper SD – 4 is an aerodynamically con-trolled, single-engine, single-pilot, two-seat all-metal low-wing UL/LSA aircraft with the side-by-side configuration of the seats. Fixed tricycle undercarriage with a front wheel. Control is doubled. The elevator and the ailerons are controlled via con-trol rods and the rudder is controlled via a control cable. Powered by Rotax 912 UL/ULS engine with fixed or variable pitch propeller.

Span 8.35 m,wing area 10.8 m2,weight with rescue system 315 kg,cruising speed 200- 220 km/h.

Tomark Aero CZ s.r.o. Zahradní 467250 64 MěšiceCzech Republic www.tomarkaero.come-mail: [email protected]


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SavageThe Savage is a tandem two−seat ultra-light aircraft of classic braced high−wing design, inspired by the lines and flying qualities of the Piper Cub family. Rugged structure of welded steel tube fuselage and empennage, covered with Dacron, and flapped all−metal wings ensure lon-gevity and ease of maintenance. Several versions and factory options available

Span 9,31 m, length 6,39 m, empty weigh 288 kg,cruising speed (75%) 170 km/h.

Zlin Aviation, s.r.o.2. května 685, Napajedla,Czech Republicwww.zlinaero.com

Piper UL CubbyA tandem two−seat high−wing braced ultralight monoplane of classic design. It features an all−wood wing and welded steel tube truss fuselage and tail surfaces. Fixed tailwheel undercarriage. Powered by Rotax 503, 912 or similar powerplants. (So far 68 aircraft built and flown.)



Trener ULA tandem two−seat low−wing ultralight, inspired by the famous Zlin Trener line. Mixed metal/wood structure, with either wooden or metal wing and welded steel tube truss, fabric covered fuselage. Fixed or retractable tailwheel undercarriage. Powered by Parma Technik (Walter) Mikron IIIC. (13 aircraft flown.)




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SonetAn all composite, side−by−side two−seat, cantilever low−wing ultralight. It has excel-lent performance and a remarkable useful load with just 45kW/60hp engine. Sonet uses the same fuselage as Sonata, but has shorter−span wings and horizontal tail surfaces. It has tricycle undercarriage with steerable nosewheel.

Span 11,70 m, length 6,40 m,wing area 10,50 m2,empty weight 265 kg,max. level speed VH 201 km/h,glide ratio14:1.

Gramex, s.r.o.Zbraslavice 399,285 21 Zbraslavice,Czech Republicwww.airsport.cze−mail: [email protected]

Tomi−Cross 5 SportTandem two−seat powered trike for hang−glider wing. Independent suspension with individually sprung wheels. Rear−wheel spats with directional fins. The frame of steel and dural tubing. Aluminium fuel tank of 38 litre capacity. Designed for Rotax, Hirth and other engines and Aeros wings.

Weight (witout engine and instruments)up to 60 kg,wheel track 1620 mm,wheelbase 1750 mm.

Tomi−Aviation - M. ŘehákBudovatelů 301,533 13 Řečany nad Labem,Czech [email protected]

S−WingA braced high−wing composite struc-ture ultralight side−by−side two−seater. Fixed tricycle undercarriage. Powered by Rotax 912UL or 912ULS engines with two−bla−ded, ground−adjustable compo-site Woodcomp propellers. (14 machines have been produced so far.)


Vladimír RajchlL. M. Pařízka 495/8,370 01 České Budějovice, Czech Republicwww.s−wing.cze−mail: [email protected]


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SonataA side−by−side two−seat, cantilever low−winged, T−tailed powered ultralight glider of composite structure. Comfortable cockpit under large forward−hinged canopy. The tandem main landing gear is retractable and has a steerable tail-wheel. The aircraft is powered by Rotax 582, special two blade composite propel-ler retracts into the nose of airplane.

Span 15,05 m, length 6,50 m,wing area 14,28 m2,empty weight 157 kg,max. level speed 185 km/h,glide ratio 29:1.


SongA single seat, carbon fibre composite air-craft for 120kg category. Powered by Bailey 200 (22 hp) engine.

Span 11,2 m, length 5,9 m,wing area 10,50 m2,empty weight 120 kg, MTOM 235 kg,maximum speed 140 km/h.


U−15 PhoenixU−15 Phoenix is a composite airplane with low wing configuration. Cockpit has a side by side seats. In future we are planning to produce not only current undercarriage with taildragger configuration, but also front wheel version. Airplane has remo-vable wing extensions and possibility of fast and easy dismantling of the wings and HTU. (10 aircraft produced so far.)

Span 15,00 m, length 6,50 m, empty weigh 295 kg,speed VH 220 km/h,cruising speed 180 km/h,glide ratio 30:1+, flight range 1500 km

Phoenix Air, s.r.o.Lochmanova 64,562 01 Ústí nad OrlicíCzech Republicwww. phoenixair.cze−mail: [email protected]


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TST−13 Junior 2009A single-seat mid-wing ultralight/LSA glider of composite structure. Tailwheel undercarriage. Powered by Rotax 447 or 503 engine and two bladed fixed/variable pitch propeller. BRS option. (5 aircrafts have been built so far).

Span 15,00 m, length 7,45 m,wing area 10,03 m2, empty weight 220 kg, max. level speed VH 160 km/h,glide ratio 30:1 at 100 km/h

Test, Comp−Let, s.r.o., org. složkaZahradní 995,594 01 Velké Meziříčí,Czech Republicwww.testandfly.cze−mail: [email protected]

Duo BanjoA two−seat braced shoulder−wing ultra-light of mixed wood/glassfibre structure, powered by Rotax 447. Retractable wood-en two−bladed ProFe propeller. Fixed two−wheel undercarriage. (10 aircraft pro-duced so far.)

Span 16,00 m, length 7,35 m,wing area 13,86 m2,empty weight 260 kg,max. level speed VH 142 km/h,glide ratio 29:1 at 103 km/h.

ProFeLeštinská 811, 549 01 Nové Město nad Metují,Czech Republicwww.profe.cze−mail: [email protected]

Banjo MHA single−seat braced high−wing ultralight of mixed wood/glassfibre structure, pow-ered by Hirth F33B. Retractable wood-en two−bladed ProFe propeller. Fixed single−wheel undercarriage. (40 aircraft produced so far.)

Span 13,30 m, length 6,30 m,wing area 10,50 m2,empty weight 157 kg,cruising speed 110 km/h,glide ratio 28:1 at 85 km/h.

ProFeLeštinská 811, 549 01 Nové Město nad Metují,Czech Republicwww.profe.cze−mail: [email protected]

CZECH AVIATION 2011UL-LSA AIRCRAFT / GLIDERS

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TST−10MC AtlasA single-seat ultralight powered glider of composite structure. The single-wheel retractable undercarriage and automa-tic connection of controls. Powered by retractable Rotax 447 unit and two-bladed fixed propeller. BRS and optimized wing-lets option. (34 machines have been manufactured so far).

Span 15,00 m, length 6,87 m,wing area 9,85 m2, empty weight 220 kg,VNE 205 km/h, glide ratio 40:1 at 110 km/h


TST−14M BonusA tandem two-seat mid-wing ultralight/LSA powered glider of composite structu-re. Two-wheel tandem undercarriage with tailwheel. Powered by retractable Rotax 503 unit and two-bladed fixed propeller. BRS and optimized winglets option. (17 machines have been manu-factured so far)

Span 17,00 m, length 8,60 mwing area 12,60 m2,empty weight 285 kg,VNE 180 km/h, glide ratio 39:1 at 110 km/h


KKB−15 (18)A single−seat experimental high performan-ce competition glider of all−composite con-struction with elliptical wing and horizontal tail for aerodynamic efficiency. Equipped with single−wheel retractable undercarria-ge and water ballast tanks of 150 liters. Flying 18m version. Motorization under development.

Span 15,00 (18,00) m, length 6,43 m,wing area 10,01 m2, MTOW 500 kg,max. speed VNE 250 km/h,glide ratio 45:1 (48) at 133 (111) km/h

Kusbach - Bartoník 769 01 HolešovOčadlíkova 36Czech Republice−mail: [email protected]


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HPH−304S/SJ SharkPHP-304S is a single−seat mid−wing, T−tailed all−composite high−performance sailplane of the FAI 18metre Class. Water ballast tanks in wing for 200 l (S)/ 180 l (SJ). The sprung and braked single main-wheel is retractable. A HpH−304SJ with an turbine engine shown here. (In series production from 2008, so far 2 (S)+12 (SJ) machines flown.)

Span 18,00 m, length 6,79 m,wing surface 11,80 m2,empty weight 295 kg, max. 600 kg,gliding ratio above 50:1 at 125 km/h.

HPH, s.r.o.Čáslavská 126, P.O.Box 112,284 01 Kutná Hora,Czech Republicwww.hph.cze−mail: [email protected]

Discus CSA single−seat mid−wing, T−tailed all−composite high−performance sailplane of the FAI Standard and Club Class. Water ballast tanks in the wing for 184 l. The sprung and braked single mainwheel is retractable, the tailwheel is not sprung. (In the Czech Republic, 331 Discus CSs have been manufactured so far.)

Span 15,00 m, length 6,58 m,wing surface 10,58 m2,empty weight 233 kg,glide ratio 42,5:1 at 100 km/h.

Schempp−Hirth,výroba letadel, spol. s r.o.U Dvořiska 1733, 565 01 Choceň,Czech Republicwww.shvl.cze−mail: [email protected]

Duo DiscusA two−seat mid−wing all−composite high−performance sailplane with a T−tail. Water ballast tanks in wing for 200 l. The sprung and braked single mainwheel is retractable, the tailwheel is not. sprung. (So far 611 of these gliders were manu-factured here.)

Span 20,00 m, length 8,62 m,wing area 16,40 m2,empty weight 410 kg,glide ratio 45:1.

Schempp−Hirth,výroba letadel, spol. s r.o.U Dvořiska 1733, 565 01 Choceň,Czech Republicwww.shvl.cze−mail: [email protected]

CZECH AVIATION 2011GLIDERS / AIRCRAFT

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HPH−304MS SharkA single−seat mid−wing, T−tailed all−composite high−performance sailplane of the FAI 18metre Class. Water ballast tanks in wing for 140 l. The sprung and braked single mainwheel is retractable. A HpH−304MS with an engine Solo 2625−01; 38 kW / 52 HP. (In series production from 2010.)

Span 18,00 m, length 6,79 m,wing surface 11,80 m2,empty weight 380 kg, max. 600 kg,gliding ratio above 50:1 at 125 km/h.

HPH, s.r.o.,Čáslavská 126, P.O.Box 112,284 01 Kutná Hora,Czech Republicwww.hph.cze−mail: [email protected]

HPH−304C WaspA single−seat mid−wing all−composite high−performance sailplane of the FAI´s Standad category with a T−tail. Water bal-last tanks in wing for 115 l. Braked single mainwheel 5x5 is retractable. 304C is easy and exellent glifder for a begginer. 2004 winner of Barron Hilton Cup. (So far 20 machines flown.)

Span 15,00 m, length 6,45 m,wing surface 9,90 m2,empty weight 235 kg,glide ratio 42,5:1 at 116 km/h.

HPH, s.r.o.,Čáslavská 126, P.O.Box 112,284 01 Kutná Hora,Czech Republicwww.hph.cze−mail: [email protected]

M1 SpeedCruiserThe M−1 SpeedCruiser is a homebuilder s kit of a new all−metal, low−wing four seater monoplane. It is designed for engines from 250 HP to 500 HP and 3-blade 1.98m diameter propeller. Its tough metal struc-ture is stressed to +6/−3 g. Kit is complete with preformed aluminium engine cowls and fairings.

Span 8,27 m, length 6,60 m,empty weight 800 kg,MTOW 1 170 kg,cruising speed 350 km/h.

High Performance AircraftInternational, s.r.o.,Lobeček 732,278 01 Kralupy nad Vltavou,Czech Republicwww.hpa−international.comwww.hpai.cze−mail: [email protected]


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EV−55 OutbackThe EV−55 Outback is the new gener-ation twin engine utility turboprop air-plane for transport of 9 to 14 passengers or corresponding cargo. The airplane has an all metal structure and is powered by PT6A−21 engines and 4−blade constant−speed propellers. Retractable lan−ding gear with anti−skid system.

Wing span 16,10 m, length 14,35 m,max. take−off weight 4 600 kg, max. cruising speed 408 km/h.

Evektor−Aerotechnik, a.s. Letecká 1384, 686 04 Kunovice, Czech Republic www.evektor.come−mail: [email protected]

VUT−100 CobraA a four−seat cantilever low−wing tour-ing monoplane of all−metal structure. Retractable tricycle undercarriage. A ”glass” cockpit with the PFD and MFD displays. Powered by Lycoming IO−580B−1A of 235 kW/315 hp with a three−bladed constant−speed propeller. (Two prototypes are flying.)

Span 10,50 m, length 8,00 m,wing area 12,20 m2,empty weight 880 kg,MTOW 1 450 kg,cruising speed 310 km/h.

Evektor−Aerotechnik, a.s.Letecká 1384, 686 04 Kunovice, Czech Republic www.evektor.come−mail: [email protected]

SM−92TE Silver FoxSM−92TE Silver Fox is a light multi−purpose STOL class aircraft operable from rugged surfaces and in most weather conditions. The all−metal airframe is a non−pressurized, high−wing monoplane with fixed tail wheel landing gear. SM−92TE is powered by Walter M 601(or new GE-H80) turboprop engine driving a 3−blade Avia AV 803 pro-peller. The aircraft is equipped with a large side sliding door enabling easy skydiving and cargo operation.

Lenght 9,97 m, height 3,1 m,max. weight 3000 kg, empty 1670 kg,max. operating speed 300 km/h,stalling speed 110 km/h,max. range 1500 km.

Orbis Avia, spol. s r.o.U kříže 632/24, CZ 158 00, Prague 5Subsidiary: International Airport Hradec Králové (LKHK)www.orbisavia.cz

CZECH AVIATION 2011AIRCRAFT

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L 410 UVP−E20All-metal, high-wing commuter aircraft for transportation of 19 passengers or cargo as well as for various other missions. The air-craft is powered by two GE M601E turbo-prop engines and is equipped with avionics made by Honeywell, Universal and Garmin. Its design provides highly reliable and efficient operation with remarkable ”hot and high” and STOL performance capabilities even on unpaved runways. Over 1100 aircraft of L 410 family have been delivered already.

Span 19,98 m, length 14,42 m,MTOW 6 600 kg,max. cruising speed 386 km/h,max. range 1 400 km.

Aircraft Industries, a.s.Na Záhonech 1177,686 04 Kunovice,Czech Republicwww.let.cze-mail: [email protected]

Z 143 LSiThe ZLIN Z 143 LSi is a multipurpose (Commercial Flights/Training/Sport/Towing) four-seat aircraft powered by single engine Lycoming IO-540-C4D5 performance reaching up to 235 HP, MTV-9-B/195-45 propeller, of 855 kg/1885 lbs weight. Simple handling, all metal struc-ture of fuselage.


Zlin Aircraft a.s. Letiště 157876581 OtrokoviceCzech [email protected]

Z 242 LThe Zlin Z 242 L is a sport and aerobatic two-seater brand Zlin aircraft powered by single engine Lycoming AEIO-360-A1B6 performance reaching up to 200 HP, MTV-9-B-C/C-188-18a propeller, of 745 kg/1642 lbs weight. Simple handling, all metal structure of fuselage.


Zlin Aircraft a.s. Letiště 157876581 OtrokoviceCzech [email protected]


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