Ellipse Spirit MH−46 Eclipse Legend UL-LSA AIRCRAFT

UL-LSA AIRCRAFT
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AeroSette
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MH−46 Eclipse
Ultralight two−seat braced high−wing monoplane. It is very controllable and features
a spacious cockpit for two side−by−side
pilots. The tricycle undercarriage is fixed,
power is provided by Rotax 912S engine,
turning a three−bladed variable−pitch propeller. (5 aircraft produced so far.)
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Span 9,80 m,
length 6,75 m,
wing area 11,30 m2,
cruising speed 190 − 250 km/h.
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AeroSette, spol. s r.o.,
Nádražní 20,
463 31 Chrastava,
Cze ch Republic
www.aerosette.eu
e−mail: [email protected]
A2 CZ
Ellipse Spirit
A side-by-side two seat low-wing aircraft
with T-tail and retractable landing gear made
of carbon fiber and honeycomb sandwich.
Powered by Rotax 912/914, UL Power
260/350 or Lycoming 233. Two prototypes
are flying and the certification process is in
progress. Basic price from 82 000 EUR.
Span 8 m (8,6 m),
length 6,55 m,
wing area 9,48 m2 (10,34 m2),
empty weight 295 - 339 kg,
(with BRS and safety fuel cells),
cruising speed 230 - 290 km/h.
A2 CZ, s.r.o.
Ráby 23
533 52 Staré Hradiště
Czech Republic
www.ellipse-spirit.com
e-mail: [email protected]
Aeropilot
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Legend
Full-composite high-wing aircraft Legend is
intended for sport, recreation and touristic
flying. This aircraft is suitable for flight training. LSA (600 kg) / UL (472 kg) / ELSA
(540 kg) versions are powered by Rotax 912
UL or 912 ULS engines. LSA (600 kg) version
is powered by Lycoming 0235 engine. The
propeller is two- or three-bladed, fixed or
adjustable. 3 prototypes have been built.
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Span: 9,06 m, Length: 7 m,
wing area: 10,54 m2,
weight: 280 – 297 kg,
max. horizontal speed: 225 km/h.
Aeropilot, s.r.o.
Jeníkovská 1815
28601 Čáslav
Czech Republic
http://www.aeropilotcz.com
e-mail: [email protected]
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CZECH AVIATION 2012
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Aerospool CZ
ULL Classic
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A two-seat, side-by-side high-wing braced
composite monoplane for both ULL and
LSA category. Powered by the Rotax 912
UL / ULS with on-ground adjustable or
constant speed propeller.
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Span 9,1 m,
lenght 6,3 m,
wing area 9,9 m2,
empty weight 285 kg,
cruising speed 180 - 220 km/h.
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Aerospool CZ, s.r.o.,
Hlavní 439,
687 25 Hluk,
Czech Republic
www.aerospool.cz
e-mail: [email protected]
AirLony
Skylane UL
A two-seat side-by-side braced high-wing
ultralight monoplane of mixed, mainly composite structure. Fixed tricycle undercarriage.
The aircraft is designed for a wide range of
use – from a trainer to a 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 62 aircraft built.)
Span: 8,95 m, length: 6,65 m,
wing area: 10,57 m2,
empty weight: 248 kg,
cruising speed: 135 - 210 km/h.
AirLony,
Nové Náměstí 702,
411 08 Štětí,
Czech Republic
www.airlony.cz
e−mail: [email protected]
AirLony
Highlander
A tandem two-seat ultralight biplane of
mixed, mainly composite structure. Fixed
tailwheel undercarriage. Highlander is
designed for leisure and joyful flying with
emphasis on safety. The aircraft is powered by Rotax 912 ULS and has increased
G-limits up to +6/-4g.
Span: 7,3 m, length: 6,05 m,
wing area: 14,3 m2,
empty weight: 230 kg,
cruising speed: 100 – 140 km/h.
AirLony,
Nové Náměstí 702,
411 08 Štětí,
Czech Republic
www.airlony.cz
e−mail: [email protected]
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Atec
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Atec 122 Zephyr
A 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 variable−pitch propellers. (220
units built so far.)
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Span 9,40 m, length 6,20 m,
wing area 10,30 m2,
empty weight 275 kg,
max. level speed VH 245 km/h.
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Atec, v.o.s.,
Opolanská 350,
289 07 Libice nad Cidlinou,
Czech Republic
www.atecaircraft.eu
e−mail: [email protected]
Atec
Atec 321 Faeta
A 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 variable−pitch propellers. The
aircraft is also certified for towing. The
Atec 322 Faeta is the LSA version. (So far
80 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 Republic
www.atecaircraft.eu
e−mail: [email protected]
Atec
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Atec 212 Solo
A single−seat ultralight airplane of composite structure. Fixed tailwheel undercarriage. Stressed for +6/−3 g. Powered by
Rotax 582 UL DCDI or 912 UL. (So far 8
machines built.)
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Span 7,50 m, length 5,26 m,
wing area 7,30 m2,
empty weight 200 kg,
max. level speed VH 245 km/h.
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Atec, v.o.s.,
Opolanská 350,
289 07 Libice nad Cidlinou,
Czech Republic
www.atecaircraft.eu
e−mail: [email protected]
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CZECH AVIATION 2012
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BRM Aero
Bristell
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UL, ELSA, LSA, RG – an all-metal twoseater powered by Rotax 912 ULS, 912 iS,
Jabiru 2200/3300 engines. Ultralight aeroplane Bristell is intended for flight training
in flight schools, glider towing and recreational flying. Thanks to large cockipt and
good ergonomy Bristell is an ideal vehicle
for long cross country flights. 25 Bristells
have been built so far.
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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.
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BRM Aero s.r.o.,
Václava Kulíška 1224,
686 05 Uherské Hradiště,
Czech Republic
www.brmaero.com
[email protected]
Czech Sport Aircraft
PS-28 Cruiser
All-metal, two-seater, low-wing LSA airplane, 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 469.
Span 8,53 m, length 6,16 m,
wing area 12,3 m2,
empty weight 370 kg,
cruising speed 200 km/h.
Czech Sport Aircraft a.s.,
Na Záhonech 1177/212,
Kunovice 686 04, Czech Republic
Phone: + 420 576 514 032
Fax: + 420 576 519 394
e-mail: [email protected]
www.czechsportaircraft.com
Czech Sport Aircraft
PS-10 Tourer
All-metal, two-seater, high-wing LSA airplane, intended for training, tourist and
patrol flights. The airframe design concept
is adjusted to this purpose – self-supporting
wing and the cockpit situated on the wing
leading edge level to provide en excellent
view 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 375 kg,
cruising speed 210 km/h.
Czech Sport Aircraft a.s.,
Na Záhonech 1177/212,
Kunovice 686 04, Czech Republic
Phone: + 420 576 514 032
Fax: + 420 576 519 394
e-mail: [email protected]
www.czechsportaircraft.com
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UL-LSA AIRCRAFT
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Direct Fly
Alto
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An all−metal cantilever low−wing ultralight
monoplane, seating two side−by−side.
Alto can be delivered in the TW version
with a tailwheel or in the TG version with
a tricycle undercarriage. Powered by Rotax
912 or Jabiru (60 kW / 80 hp to 90 kW /
120 hp range). Also available as a kit for
homebuilders in various stages of assembly. (41 aircraft have been built so far)
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Span 8,20 m, length 6,25 m,
wing area 10,50 m2,
empty weight 285 kg,
cruising speed 195 km/h.
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Direct Fly, s.r.o.,
Cihelní 573,
687 25 Hluk,
Czech Republic
www.directfly.cz
e−mail: [email protected]
Direct Fly
Argo
Classical all-metal high-wing ultralight
or LSA aircraft, with side-by-side seats,
powered 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 Republic
www.directfly.cz
e−mail: [email protected]
Distar
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UFM−13 Lambada
A side-by-side two-seat, mid-wing ultralight of composite structure. Fixed tricycle
or tailwheel undercarriage. Powered by
Rotax 912 UL, ULS or Jabiru 2200 engines, with fixed or variable-pitch propeller.
The wing may be fitted with wingtip extensions, increasing the span to 15 m. (About
140 aircraft in the UFM-11-13 version have
been produced so far.)
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Span 13,0 0 m, length 6,60 m,
wing area 12,60 m2,
empty weight 265 − 280 kg,
cruising speed 135 km/h.
Production division:
Company headquarters:
Distar − Air,
Distar CZ, a.s.,
U Letiště 1381
562 01 Ústí nad Orlicí
Czech Republic
e-mail: [email protected]
www.sambaXXL.com
1. máje 228
504 01 Nový Bydžov
Czech Republic
e-mail: [email protected]
www.distar.cz
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CZECH AVIATION 2012
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Distar
Samba XXL
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A low-wing, composite side-by-side twoseat ultra-light monoplane. Fixed tricycle
undercarriage. Powered by Rotax 912UL
or ULS engines, with fixed or variablepitch propeller. Since 2010 it is manufactured with a modified cockpit, providing
great comfort in the cabin. (More than 100
aircraft have been produced so far.)
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Span 10,00 m, length 6,00 m,
wing area 8,90 m2,
empty weight 260 kg,
cruising speed 220 km/h.
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Production division:
Company headquarters:
Distar − Air,
Distar CZ, a.s.,
U Letiště 1381
562 01 Ústí nad Orlicí
Czech Republic
e-mail: [email protected]
www.sambaXXL.com
1. máje 228
504 01 Nový Bydžov
Czech Republic
e-mail: [email protected]
www.distar.cz
Dova Aircraft
DV−1 Skylark
All-metal side-by-side two-seater aircraft
complying with Ultralight/AULA/LSA/ELSA
regulations. The tapered low wing equipped
with winglets and the T-tail present unique
design in this cathegory. It has fixed tricycle
undercarriage and is powered by Rotax
912UL/ULS with fixed or variable-pitch propeller. Available in certified towing version
for gliders with MTOM 510 kg. So far 175
aircraft have been produced. Price from 59
900 Euro.
Span 8,13 m, length 6,62 m,
wing area 9,44 m2,
empty weight 285 kg,
cruising speed 215 km/h.
Dova Aircraft, s.r.o.,
Kirilovova 115,
739 21 Paskov, Czech Republic
www.dovaaircraft.cz
e−mail: [email protected]
Eurodisplay
SR−01 Magic
Tandem two−seat low−wing all−metal
monoplane with tricycle fixed undercarriage. Powered by Rotax 912ULS with
a three−blade composite Woodcomp propeller. The aircraft is designed for the
UL and LSA category. 2 prototypes have
been built 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 Republic
www.aeromagic.cz
e−mail: [email protected]
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Evektor−Aerotechnik
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EuroStar SL / SLW
A side−by−side two−seat cantilever low−wing
advanced ultralight aircraft of all-metal
structure. Fixed tricycle undercarriage.
Powered by Rotax 912UL or ULS engines, with fixed or variable pitch propeller.
EuroStar SLW version uses LSA airframe
with a wet wing and range of 1300 km.
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Span 8,10 m, length 5,98 m,
wing area 9,84 m2,
weight 264 kg,
cruising speed 210 − 245 km/h.
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Evektor−Aerotechnik, a.s.,
Letecká 1384,
686 04 Kunovice,
Czech Republic
www.evektoraircraft.com
e−mail: [email protected]
Evektor−Aerotechnik
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
category. Powered by Rotax 912ULS /
912 iS engines with fixed or variable-pitch
propeller. Fixed tricycle undercarriage.
Altogether 1100+ aircraft of the EuroStar/
SportStar line have been built.
Span 8,65 m, length 5,98 m,
wing area 10,47 m2,
weight 307 kg,
cruising speed 205 − 215 km/h.
Evektor−Aerotechnik, a.s.,
Letecká 1384,
686 04 Kunovice,
Czech Republic
www.evektoraircraft.com
e−mail: [email protected]
Evektor−Aerotechnik
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SportStar RTC
An all-metal side−by−side two−seat training airplane designed according to new
EASA CS-LSA regulations using airframe
from EASA JAR-VLA certified trainer called
Harmony. Powered by Rotax 912S engine,
with fixed or variable-pitch propeller. Fixed
tricycle undercarriage.
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Span 8,65 m, length 5,98 m,
wing area 10,47 m2,
weight 339 kg,
cruising speed 205 − 215 km/h.
Evektor−Aerotechnik, a.s.,
Letecká 1384,
686 04 Kunovice,
Czech Republic
www.evektoraircraft.com
e−mail: [email protected]
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CZECH AVIATION 2012
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Evektor−Aerotechnik
Harmony LSA
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A side−by−side two−seat cantilever lowwing advanced UL / LSA aircraft of allmetal structure. Fixed tricycle undercarriage. Powered by Rotax 912ULS, 912iS or
914UL engines, with fixed or variable-pitch
propeller. The Harmony has tapered wing,
120 l wing tanks providing 1300 km range
and outstanding cockpit spaciousness.
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Span 9,25 m, length 6,11 m,
wing area 9,84 m2,
weight 310 kg,
cruising speed 210 − 245 km/h.
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Evektor−Aerotechnik, a.s.,
Letecká 1384,
686 04 Kunovice,
Czech Republic
www.evektoraircraft.com
e−mail: [email protected]
Flying Machines
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 useful load of 190 kg. It is capable of towing
gliders 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 Republic
www.flyingmachines.cz
e−mail: [email protected]
Gramex
Sonet
An all-composite, side−by−side two−seat,
cantilever low−wing ultralight. It has excellent performance and a remarkable useful
load with just 45 kW / 60 hp engine. Sonet
uses the same fuselage as Sonata, but
has shorter−span wings and horizontal tail
surfaces. It has tricycle undercarriage with
steerable nosewheel. (3 machines have
been produced so far.)
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 ratio 14:1.
Gramex, s.r.o.,
Zbraslavice 399,
285 21 Zbraslavice, Czech Republic
www.airsport.cz
e−mail: [email protected]
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Gramex
Sonata
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A 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 tailwheel.
The aircraft is powered by Rotax 582, special
two blade composite propeller retracts into
the nose of airplane. (3 machines have been
produced so far.)
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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.
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Gramex, s.r.o.
Zbraslavice 399,
285 21 Zbraslavice, Czech Republic
www.airsport.cz, e−mail: [email protected]
Gramex
Song
A single-seat, carbon-fiber composite aircraft for 120 kg category. Powered by
Bailey 200 (22 hp) / Verner VC 360 (35 hp)
engines.
Span 11,2 / 7,5 m, length 5,9 m,
wing area 10,50 m2,
empty weight 120 kg, MTOM 235 kg,
maximum speed 140 km/h.
Gramex, s.r.o.,
Zbraslavice 399,
285 21 Zbraslavice,
Czech Republic
www.airsport.cz
e−mail: [email protected]
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Ivanov Aircraft
ZJ−Viera
The 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
covered in Ceconite fabric. Powered
by a single−cylinder Flyengine F200
two−stroke of 19 kW / 26 hp. 16 aircraft
have been built so far.
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Span 7,50 m, length 5,00 m,
wing area 9,00 m2,
empty weight 77 kg,
cruising speed 103 km/h.
Ivanov Aircraft s.r.o.,
Tř. E. Beneše 1561,
500 12 Hradec Králové,
Czech Republic
www.IvanovAero.cz
e−mail: [email protected]
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CZECH AVIATION 2012
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Jaroslav Sedláček UL-jih
E100 Evolution
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A side−by−side two−seat, cantilever
high−wing monoplane of composite
structure. Wing with slotted flaps, fixed
or retractable tricycle undercarriage.
Powered by Rotax 912UL (ULS), with
a ground−adjustable DUC, or variable−pitch
Woodcomp SR 3000/2W propeller.
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Span 9,12 m, length 6,9 m,
wing area 11 m2,
weight 294 kg,
cruising speed 243 km/h.
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Jaroslav Sedláček UL-jih,
Linecká 829,
382 41 Kaplice,
Czech Republic
www.uljih.cz
www.fascination.aero
e−mail: [email protected]
Jaroslav Sedláček UL-jih
F100 Fascination
A 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), with
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 243 km/h.
Jaroslav Sedláček UL-jih,
Linecká 829,
382 41 Kaplice,
Czech Republic
www.uljih.cz
www.fascination.aero
e−mail: [email protected]
Jaroslav Sedláček UL-jih
Colibri
Easy built aircraft, with two side-by-side seats,
braced wing, powered by Rotax 503 UL/DCDI
in pushing configuration. Sprung landing gear
with a nose wheel. Suitable for beginners and
for recreational flying. Fuselage - aluminum
and steel tubes. Wings - aluminum tubes, PU
ribs, aluminum structure ailerons, steel support structure with thin wall steel tubes. Wing
fuel tanks optional.
Span 9,44 m, length 5,5 m,
wing area 12 m2,
weight 195 kg,
speed range 62 - 140 km/h.
Jaroslav Sedláček UL-jih,
Linecká 829, 382 41 Kaplice,
Czech Republic
www.uljih.cz, www.fascination.aero
e−mail: [email protected]
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UL-LSA AIRCRAFT
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Jaroslav Sedláček UL-jih
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Sunwheel UL
A nice retro style biplane, dual controls,
four stroke engine Rotax 912 UL, built with
high level quality materials. For advanced
pilots and for extraordinary flights.
Engine Rotax 912 UL. Fuselage - argonwelded steel truss structure covered with
canvas, laminated spans. Wings - aluminum tubes, PU ribs, covered with canvas,
ailerons inside of the profile.
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Span 7,5 m, length 5,7 m,
wing area 16 m2,
empty weight 251 kg,
cruising speed 130 km/h.
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Jaroslav Sedláček UL-jih
Linecká 829,
382 41 Kaplice,
Czech Republic
www.uljih.cz, www.fascination.aero
e−mail: [email protected]
Jihlavan Airplanes
Skyleader 600
The Skyleader 600 is an all-metal two-seat
low-wing UL/LSA aircraft with a tapered
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 mainly for
recreational flying, pilot training and special operations. Engine type: Rotax 912 UL,
ULS, 914UL or 912iS.
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.
Jihlavan Airplanes, s.r.o.,
Znojemská 826/64,
586 01 Jihlava,
Czech Republic
www.skyleader.aero
Jihlavan Airplanes
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Skyleader 200 / 500
The Skyleader 200/500 is an all-metal
two-seat low-wing UL/LSA aircraft with
a tapered 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 mainly for recreational flying, pilot training and
special operations. Engine type: Rotax
912 UL, ULS, 914UL or 912iS. 200+ aircraft have been built so far.
R
D
F
A
Span 9,90 m, length 7,0 m,
wing area 11,85 m2,
empty weight 298 / 313 kg,
MTOM 450 / 580 kg,
cruising speed 215 km/h.
Jihlavan Airplanes, s.r.o.
Znojemská 826/64,
586 01 Jihlava, Czech Republic
www.skyleader.aero
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CZECH AVIATION 2012
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Jihlavan Airplanes
Skyleader 100
T
F
The Skyleader 100 is an all-metal one-seat
low-wing ultralight aircraft with a rectangular or tapered wing. The aircraft has a conventional “taildragger” landing gear with
a fixed gear option only. The aircraft is
designated mainly for recreational flying.
Engine type: Rotax 503UL, 582UL, HKS
700. One prototype has been built so far.
A
R
Span 6,9 m, length 5,6 m,
wing area 8,82 m2,
empty weight 210 kg,
cruising speed 140 km/h.
D
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T
F
T
F
A
A
R
R
D
D
T
T
F
F
F
A
A
R
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Jihlavan Airplanes, s.r.o.,
Znojemská 826/64,
586 01 Jihlava,
Czech Republic
e-mail: [email protected]
www.skyleader.aero
Jihlavan Airplanes
Skyleader GP One
The Skyleader GP ONE is carbon-composite two-seat, high-wing ultralight aircraft
with a monocoque construction. The aircraft has a fixed tricycle towed landing
gear with a steerable nose wheel. This aircraft is designated mainly for pilot training
and low-cost flying. Two prototypes have
been produced.
Engine type: Rotax 912 UL.
Span 10,2 m, length 6,25 m,
wing area 11,17 m2,
empty weight 280 kg,
cruising speed 193 km/h.
Jihlavan Airplanes, s.r.o.,
Znojemská 826/64,
586 01 Jihlava,
Czech Republic
www.skyleader.aero
JMB Aircraft
VL−3
A 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.
Design:
Manufacturer:
Vanessa air, s.r.o.,
JMB Aircraft, s.r.o.
Toulovcovo nám. 1163,
570 01 Litomyšl,
Czech Republic
www. vanessaair.cz
e− mail: [email protected]
Nádražní 635,
565 01 Choceň
Czech Republic
www.jmbaircraft.com
[email protected]
17
UL-LSA AIRCRAFT
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Jora
Jora
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F
A composite−structure, braced high−wing
side−by−side two−seat ultralight. Fixed
tricycle undercarriage. Powered by a choice of Jabiru 2200, Rotax 912UL or Rotax
582 engines. The propeller is a two−blade,
ground−adjustable Woodcomp. (133 aircraft have been built, including kits)
A
R
Span 9,80 m, length 6,05 m,
wing area 11,40 m2,
weight 262 − 275 kg,
max. level speed VH 186 km/h.
D
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F
T
F
A
A
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R
D
D
D
Jora, spol. s r.o.
565 42 Vraclav,
Czech Republic,
www.jora.cz
e−mail: [email protected]
Kubíček Aircraft
M−2 Scout
A side-by-side two-seater low-wing aircraft
of classic shapes and “retro” look, available in UL and LSA versions. Powered
by Rotax 912 with fixed or variable-pitch
propeller. Fixed tricycle undercariage,
nosewheel 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 2b,
614 00 Brno,
Czech Republic
www.kubicekaircraft.cz
e-mail: [email protected]
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18
A
R
T
F
Phoenix Air
U−15 Phoenix
A composite structure, low-wing configuration, two-seat, side-by-side, LSA/UL
motorglider. Tail-dragger with fixed undercarriage. Powered by Rotax 912 or Jabiru
2200 engines. Propeller is two blade feathering from Woodcomp.
F
A
Span 15,00 m, length 6,50 m,
empty weigh 300 kg,
wing area 12,36 m2,
speed VH 220 km/h,
cruising speed 180 km/h,
glide ratio 32:1+
R
D
Phoenix Air, s.r.o.,
Lochmanova 64,
562 01 Ústí nad Orlicí,
Czech Republic
www. phoenixair.cz
e−mail: [email protected]
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CZECH AVIATION 2012
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Phoenix Air
D-14 PhoEnix
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F
A composite structure, mid-wing configuration, two seat, side-by-side, electric
motorglider. The tail-dragger type landing
gear is retractable. Powered by a Kral
44 kW electric engine with a two-blade
adjustable/feathering propeller produced
by Phoenix Air.
A
R
Span 14,46 m, length 6,50 m,
empty weigh 300 kg,
wing area 10,08 m2,
speed VH 220 km/h,
cruising speed 180 km/h,
glide ratio 36:1
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T
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T
F
A
A
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R
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D
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T
F
F
F
A
A
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R
D
D
Phoenix Air, s.r.o.,
Lochmanova 64,
562 01 Ústí nad Orlicí,
Czech Republic
www.phoenixair.cz
e−mail: [email protected]
ProFe
Banjo MH
A single−seat braced high−wing ultralight of mixed wood/fiber-glass structure, powered by Hirth F33B. Retractable
wooden two−blade 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.
ProFe,
Leštinská 811,
549 01 Nové Město nad Metují,
Czech Republic
www.profe.cz
e−mail: info@profe .cz
ProFe
Duo Banjo
A two−seat braced high−wing ultralight
of mixed wood/fiber-glass structure,
powered by Rotax 447. Retractable wooden two−blade ProFe propeller. Fixed
two−wheel undercarriage. (10 aircraft produced 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.
ProFe,
Leštinská 811,
549 01 Nové Město nad Metují,
Czech Republic
www.profe.cz
e−mail: [email protected]
19
UL-LSA AIRCRAFT
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Rokospol
NG4
T
F
The aircraft is unique by its construction,
where emphasis is put on great flying features, maximum safety and passenger’s
comfort (the widest cabin in its category),
on achievement of high traveling speed
and to ensure maximal economic operation and maintenance cost. The aircraft’s
characteristic is long lifetime given by its
modern construction and quality of manufacturing process.
A
R
Span 8,13 m, length 6,45 m,
wing area 10,5 m2,
cruising speed 220 - 240 km/h.
D
T
F
T
F
A
A
R
R
D
D
D
Rokospol a.s.,
Kaňovice 101,
763 41 Kaňovice,
Czech Republic
www.rokospolaviation.com
[email protected]
Shark.Aero CZ
Shark
A tandem two-seat high performance UL/
LSA/ELA low-wing with all-composite, mostly carbon airframe. Retractable undercarriage for MTOM 472,5 kg UL and 600 kg experimental versions, fixed u/c and LSA/ELA
under development. Powered by Rotax 912
ULS, variable-pitch propeller. Finished flying
UL prototype with retractable undercarriage,
starting of serial production.
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,
optimal cruising speed 250 - 270 km/h,
flight range (100 l tanks) 1400 km.
Shark.Aero CZ s.r.o.,
Mladá 837,
687 25 Hluk, Czech Republic
www.shark.aero, e-mail: [email protected]
Spacek
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A
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SD-1 Minisport
A single-seat cantilever low-wing UL/LSA
aircraft of mixed wood/composite construction with fixed undercariage in taildragger or tricycle configuration. It can
be powered by engines in the range of
23 - 50 hp. Also suitable for amateur construction. (50 kits and aircraft have been
produced so far)
R
D
F
A
Span 6 m, lenght 4,3 m
Wing area 6 m2
empty weight 120 kg
gross weight 240 kg
max. speed in horizontal flight 200 km/h.
Spacek s.r.o.
Lesní 25,
695 01 Hodonín,
Czech Republic
www.sdplanes.com
e-mail:[email protected]
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CZECH AVIATION 2012
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Test, Comp−Let
T
F
TST−13 Junior 2009
A single-seat mid-wing ultralight/LSA
glider of composite structure. Tailwheel
undercarriage. Powered by Rotax 447
or 503 engine and two-blade fixed/variablepitch propeller. BRS option. (5 aircraft
have been built so far).
A
R
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.
D
T
T
F
T
F
A
A
R
R
D
D
T
T
F
F
F
A
A
R
R
D
D
Test, Comp−Let, s.r.o., org. složka
Zahradní 995,
594 01 Velké Meziříčí,
Czech Republic
www.testandfly.cz
e-mail: [email protected]
Test, Comp−Let
TST−10MC Atlas
A single-seat ultralight powered glider
of composite structure. Single-wheel
retractable undercarriage and automatic connection of controls. Powered by
retractable Rotax 447 unit and two-blade
fixed propeller. BRS and optimized winglets optional. (34 aircraft 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.
Test, Comp−Let, s.r.o., org. složka,
Zahradní 995,
594 01 Velké Meziříčí,
Czech Republic
www.testandfly.cz
e-mail: [email protected]
Test, Comp−Let
TST−14M Bonus
A tandem two-seat mid-wing ultralight/LSA
powered glider of composite structure.
Two-wheel tandem undercarriage with tailwheel. Powered by retractable Rotax 503
unit and two-blad fixed propeller. BRS and
optimized winglets optional. (17 machines
have been manufactured so far)
Span 17,00 m, length 8,60 m,
wing area 12,60 m2,
empty weight 285 kg,
VNE 180 km/h,
glide ratio 39:1 at 110 km/h.
Test, Comp−Let, s.r.o., org. složka,
Zahradní 995,
594 01 Velké Meziříčí,
Czech Republic
www.testandfly.cz
e-mail: [email protected]
21
UL-LSA AIRCRAFT
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F
TL-ultralight
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F
TL-2000 Sting S4
Aerodynamically and visually enhanced version of the successful Sting brings even
better performance and appearance. The
Sting S4 is a two seater low-wing aircraft
made from carbon fiber. Powered by a Rotax
912UL, 912ULS or 912iS with a groundadjustable or a new variable-pitch threeblade PowerMax propeller. (more than 500
Stings have been manufactured so far)
A
R
Span 9,11 m, length 6,2 m,
wing area 10,52 m2,
empty weight 297 kg,
max. horizontal speed 270 km/h.
D
T
F
T
F
A
A
R
R
D
D
D
TL-ultralight s.r.o.,
Letiště − budova č. 84,
503 41 Hradec Králové, Czech Republic
www.tl-ultralight.cz
e-mail: [email protected]
TL-ultralight
TL-3000 Sirius
A side-by-side two-seat light sport highwing carbon composite aircraft with
fixed tricycle undercarriage. Powered by
a Rotax 912UL, 912ULS or 912iS with
a ground-adjustable or new variable-pitch
three-blade PowerMax propeller. TL 3000
Sirius – the perfect partner for fun flying
without limits. (more then 80 Siriuses have
been manufactured so far)
Span 9,40 m, length 6,75 m,
wing area 11,15 m2,
empty weight 297 kg,
max. horizontal speed 230 km/h.
TL-ultralight s.r.o.,
Letiště − budova č. 84,
503 41 Hradec Králové, Czech Republic
www.tl-ultralight.cz
e-mail: [email protected]
TL-ultralight
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TL-2000 Sting RG
A side-by-side two-seat cantilever lowwing light sport aircraft of composite construction with fixed or retractable tricycle
undercarriage. Powered by a Rotax
912UL, 912ULS or 912iS with a groundadjustable or a new variable-pitch threeblade PowerMax propeller.
R
D
F
A
Span 8,44 m, length 6,19 m,
wing area 9,81 m2,
empty weight 297 kg,
max. horizontal speed 270 km/h.
TL-ultralight s.r.o.,
Letiště − budova č. 84,
503 41 Hradec Králové, Czech Republic
www.tl-ultralight.cz
e-mail: [email protected]
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CZECH AVIATION 2012
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Tomark Aero CZ
Viper SD-4
T
F
Viper SD-4 is an all-metal, side-by-side
low-wing two-seater UL/LSA aircraft, ideal
for travelling, flight schools, tourism and
glider towing. Fixed tricycle landing gear
with a nose wheel. Powered by a Rotax 912
UL/ULS engine with fixed or variable-pitch
propeller. Great equipment, excellent flight
characteristics specially designed to please
aviation enthusiasts and fans of modern
design.
A
R
Span 8,35 m, length 6,40 m,
wing area 10,8 m2
MTOM: 472,5 kg / 600 kg,
Cruising speed 220 km/h.
D
T
T
F
T
F
A
A
R
R
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D
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T
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F
F
A
A
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Tomark Aero CZ s.r.o.,
Zahradní 467,
250 64 Měšice, Czech Republic
www.tomarkaero.com, www.vipersd4.com
e-mail: [email protected]
Tomáš Podešva
Tulák Dandy
A 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 undercarriage. Powered by Rotax 503 or 912 and similar powerplants. (so far 68 aircraft flying)
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 letadel,
Újezd u Uničova 87,
783 96,
Czech Republic
www.podesva−air.com
e−mail: [email protected]
Tomáš Podešva
Piper UL Cubby
A 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)
Span 8,68 m, length 6,40 m,
wing area 10,80 m2,
empty weight 292 kg,
cruising speed 165 km/h.
Tomáš Podešva výroba a opravy UL letadel,
Újezd u Uničova 87,
783 96,
Czech Republic
www.podesva−air.com
e−mail: [email protected]
23
UL-LSA AIRCRAFT
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F
Tomáš Podešva
Trener UL
T
F
A 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 flying)
A
R
Span 8,68 m, length 6,40 m,
wing area 10,80 m2,
empty weight 292 kg,
cruising speed 165 km/h.
D
T
F
T
F
A
A
R
R
D
D
D
Tomáš Podešva výroba a opravy UL letadel,
Újezd u Uničova 87,
783 96,
Czech Republic
www.podesva−air.com
e−mail: [email protected]
Vladimír Rajchl
S−Wing
A braced high−wing composite structure
ultralight side−by−side two−seater. Fixed
tricycle undercarriage. Powered by Rotax
912UL or 912ULS engines with two−blade,
ground−adjustable compo­site Woodcomp
propellers. (14 machines have been produced so far)
Span 10,20 m, length 6,29 m,
wing area 12,68 m2,
empty weight 296 kg,
cruising speed 160 km/h.
Vladimír Rajchl
L. M. Pařízka 495/8,
370 01 České Budějovice,
Czech Republic
www.s−wing.cz
e−mail: [email protected]
Wolfsberg Letecká Továrna
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24
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F
Sparrow
This tandem two-seater ultralight has all
composite structure with excellent all–
around view. Entrance to the cockpit is the
same as to a car. The aircraft is p owered
by Rotax 582 with a three-blade groundadjustable propeller.
F
A
Span 9,2 m, lenght 7,0 m,
Weight 265 -270 kg, MTOM 450 kg
Max. level speed (VH) 180 km/h
R
D
Wolfsberg Letecká Továrna, s.r.o.,
Beranových 65,
199 02 Praha 9 - Letňany,
Czech Republic
[email protected]
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TRIKES
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Zlin Aviation
Savage
T
F
The Savage is a tandem two−seat ultralight 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 longevity and ease of maintenance. Several
versions and factory options available.
A
R
Span 9,31 m, length 6,39 m,
empty weigh 288 kg,
cruising speed (75%) 170 km/h.
D
T
T
F
T
F
A
A
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R
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D
T
T
F
F
F
A
A
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R
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D
Zlin Aviation, s.r.o.,
2. května 685, Napajedla,
Czech Republic
www.zlinaero.com
Flying Machines
FM−301 Stream
FM-301 Stream is an all-composite two
seater microlight trike of frameless loadbearing construction. The aerodynamic
shape of the machine makes it quite easy
and comfortable to handle both on ground
and in the air. Unbeatably large baggage
compartment is situated inside the trike’s
body. It easily accommodates bulky camping equipment and gear necessary for
longer travel.
Weight ready to fly (Rotax 912, Rescue
system, Wing CZ 15,4) 223 kg.
Flying Machines, s.r.o.,
Rasošky 132,
55221 Rasošky,
Czech Republic
www.flyingmachines.cz
e−mail: [email protected]
Tomi−Aviation
Tomi−Cross 5 Sport
A tandem two−seat powered trike for a
hang−glider wing. Independent suspension
with individually sprung wheels. Rear−wheel
spats with directional fins. The frame is made
of steel and dural tubing. Aluminium fuel
tank has a 38 litre capacity. Designed for
Rotax, Hirth and other engines and Aeros
wings.
Weight (without engine and instruments)
up to 60 kg,
wheel track 1620 mm,
wheelbase 1750 mm.
Tomi−Aviation - M. Řehák,
Budovatelů 301,
533 13 Řečany nad Labem,
Czech Republic
www.rogalo.info
[email protected]
25
SAILPLANES
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Ultralight Design
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F
Atos Trike VR 190
High performance and specific construction of ATOS gliders bring you great benefits and unbelievably variability of the use.
Light, full-composite trike powered by a
paramotor engine, specially designed for
serial ATOS family, give you possibility to
fly in the thermals (glide ratio 19) or recreational flying without the necessity of big
airports.
A
R
Span 13,8 m,
wing area 14,7 m2,
min. speed 37 km/h,
cruising speed 50-90 km/h,
empty weight 93,5 kg.
D
T
F
T
F
A
A
R
R
D
D
D
Ultralight Design s.r.o.,
Žitavská 361/II,
471 54 Cvikov, Czech Republic
www.ultralightdesign.cz
[email protected]
HPH
HPH−304S/SJ Shark
PHP-304S is a single−seat mid−wing,
T−tailed all−composite high−performance
sailplane of the FAI 18-meter Class. Water
ballast tanks in wings for 200 l (S)/ 180 l
(SJ). The sprung and braked single main
wheel is retractable. A HpH−304SJ with
a turbine engine is shown here. (in serial
production since 2008, so far 2 „S“ and 12
„SJ“ gliders are flying)
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 Republic
www.hph.cz, e−mail: [email protected]
HPH
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F
HPH−304MS Shark
A single−seat
mid−wing,
T−tailed
all−composite high−performance sailplane
of the FAI 18-meter Class. Water ballast
tanks in wings for 140 l. The sprung and
braked single mainwheel is retractable.
A HpH−304MS with Solo 2625−01 38 kW
/ 52 hp engine. Currently there are more
than 100 of all versions of the 304 flying.
R
D
F
A
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 Republic
www.hph.cz, e−mail: [email protected]
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CZECH AVIATION 2012
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HPH
T
F
HPH−304C Wasp
A single−seat mid−wing all−composite
high−performance sailplane of the FAI´s
Standad category with a T−tail. Water ballast tanks in wing for 115 l. Braked single mainwheel 5x5 is retractable. 304C is
an easy and exellent glifder for a begginer. 2004 winner of Barron Hilton Cup.
Currently there are more than 100 of all
versions of the 304 flying.
A
R
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.
D
T
T
F
T
F
A
A
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R
D
D
T
T
F
F
F
A
A
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D
HPH, s.r.o.,
Čáslavská 126,
P.O.Box 112,
284 01 Kutná Hora,
Czech Republic
www.hph.cz, e−mail: [email protected]
Kusbach - Bartoník
KKB−15 (18)
A single−seat experimental high performance competition glider of all−composite
construction with elliptical wing and horizontal tail for aerodynamic efficiency.
Equipped with single−wheel retractable
undercarriage and water ballast tanks for
150 liters. Flying 18m version. Motorization
under development. (2 gliders have been
manufactured so far)
Span 15,00 (18,00) m, length 6,43 m,
wing area 10,01 m2, MTOM 500 kg,
max. speed VNE 250 km/h,
glide ratio 45:1 (48:1) at 133 (111) km/h.
Kusbach - Bartoník,
769 01 Holešov,
Očadlíkova 36,
Czech Republic
e−mail: [email protected]
Schempp−Hirth
Duo Discus
A 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 manufactured in CR)
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 Republic
www.shvl.cz
e−mail: [email protected]
27
GENERAL AVIATION
D
A
R
T
F
Schempp−Hirth
Discus CS
T
F
A single−seat
mid−wing,
T−tailed
all−composite high−performance sailplane
of the FAI Standard and Club Class. Water
ballast tanks in the wings 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)
A
R
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.
D
T
F
T
F
A
A
R
R
D
D
D
Schempp−Hirth,
výroba letadel, spol. s r.o.,
U Dvořiska 1733,
565 01 Choceň,
Czech Republic
www.shvl.cz
e−mail: [email protected]
Aircraft Industries
L 410 UVP−E20
All-metal, high-wing commuter aircraft for
transportation of 19 passengers or cargo as
well as for various other missions. The aircraft is powered by two GE M601E turboprop
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,
MTOM 6600 kg,
max. cruising speed 386 km/h,
max. range 1400 km.
Aircraft Industries, a.s.,
Na Záhonech 1177,
686 04 Kunovice, Czech Republic
www.let.cz, e-mail: [email protected]
D
28
A
R
T
F
Evektor−Aerotechnik
VUT−100 Cobra
A a four−seat cantilever low−wing touring 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−blade
constant−speed propeller. (Two prototypes
are flying.)
R
D
F
A
Span 10,50 m, length 8,00 m,
wing area 12,20 m2,
empty weight 880 kg,
MTOM 1450 kg,
cruising speed 310 km/h.
Evektor−Aerotechnik, a.s.,
Letecká 1384,
686 04 Kunovice,
Czech Republic
www.evektor.com
e−mail: [email protected]
T
CZECH AVIATION 2012
D
A
R
T
F
Evektor−Aerotechnik
EV−55 Outback
T
F
The EV−55 Outback is the new generation twin engine utility turboprop airplane for transport of 9 to 14 passengers
or equivalent cargo. The airplane has
an all metal structure and is powered
by PT6A−21 engines with 4−blade
constant−speed propellers. Retractable
landing gear with anti−skid system.
A
R
Span 16,10 m,
length 14,35 m,
max. take−off weight 4600 kg,
max. cruising speed 408 km/h.
D
T
T
F
T
F
A
A
R
R
D
D
T
T
F
F
F
A
A
R
R
D
D
Evektor−Aerotechnik, a.s.,
Letecká 1384,
686 04 Kunovice,
Czech Republic
www.evektor.com
e−mail: [email protected]
High Performance Aircraft
M1 SpeedCruiser
The M−1 SpeedCruiser is a homebuilders‘
kit of a new all−metal, low−wing four seater
monoplane. It is designed for engines
from 250 to 500 hp and 3-blade 1,98 m
diameter propeller. Its tough metal structure 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,
MTOM 1170 kg,
cruising speed 350 km/h.
High Performance Aircraft
International, s.r.o.,
Lobeček 732,
278 01 Kralupy nad Vltavou,
Czech Republic
www.hpa−international.com, www.hpai.cz
e−mail: [email protected]
Orbis Avia
SM-92T Silver Fox
SM-92T Silver Fox is a single turboprop,
all-metal, 7 seats aircraft (PART 23, Normal
Category). Silver Fox is able to operate on
remote airfields and untreated surfaces
due to its robust construction. The aircraft
has STOL features. Powerplant: 1x Walter
M601F with Avia V508E propeller.
Span 14,86 m, lenght 9,97 m,
MTOM 3000 kg, empty 1670 kg,
max. payload 900 kg,
max. operating speed 300 km/h,
stall speed KCAS-MTOM 113 km/h,
max. range 1150 km,
climb rate 9,5 m/s.
Orbis Avia, spol. s r.o.
Letiště Hradec Králové, Hangár č. 165,
503 41 Hradec Králové,
Czech Republic
www.orbisavia.cz
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ENGINES
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Zlin Aircraft a.s.
T
F
Z 143 LSi Genius
The ZLIN Z 143 LSi is a multipurpose
(commercial/training/sport/towing) fourseat aircraft powered by single engine
Lycoming IO-540-C4D5 with performance up to 235 hp and MTV-9-B/19545 propeller, with empty weight 855 kg
/ 1885 lbs. Simple handling, all metal
structure of fuselage. Garmin’s G950
avionics suite.
A
R
Span 10,14 m, length 7,58 m,
wing area 14,77 m2,
empty weight 855 kg,
cruising speed 243 km/h.
D
T
F
T
F
A
A
R
R
D
D
D
Zlin Aircraft a.s.,
Letiště 1578,
76581 Otrokovice,
Czech Republic
www.zlinaircraft.eu
[email protected]
Zlin Aircraft a.s.
Z 242 L Guru
The new ZLIN Z 242 L is a sport and
aerobatic two-seater brand ZLIN aircraft
powered by a single engine Lycoming
AEIO-360-A1B6 performance reaching up
to 200 hp with MTV-9-B-C/C-188-18a propeller, of 745 kg/1642 lbs weight. Simple
handling, all metal structure of fuselage.
Garmin’s G500 avionics suite.
Span 9,34 m, length 6,94 m,
wing area 13,86 m2,
empty weight 745 kg,
cruising speed 227 km/h.
Zlin Aircraft a.s.,
Letiště 1578,
76581 Otrokovice
Czech Republic
www.zlinaircraft.eu
[email protected]
Fly Engine
D
30
A
R
T
F
F-200
The lateast model of this engine is a result
of 6 years of continous development and
testing. It is a powerful air cooled twostroke engine with high reliability, specially
designed for paramotors and small, light
powered paraglider trikes.
Volume power
max. rpm bore
stroke reduction complete weight Starter F
A
200 cc,
27 hp,
7900,
66 mm
56 mm
2,5/3,1
14 kg
electric
R
D
Fly Engine,
Viktor Procházka
Tatiná 32, 330 11 p. Třemošná,
Czech Republic
www.flyengines.com
[email protected]
T
CZECH AVIATION 2012
D
A
R
T
F
Parma − Technik, s.r.o.
Mikron III
T
F
The Mikron III is an inverted in−line
four−cylinder four−stroke, OHV petrol aircooled engine, with a downdraught carburettor. It is produced in several versions −
for lightplanes (A, AE, B) and for ultralights
(AUL, BUL).
A
R
Left−hand turning
cylinder bore
90 mm,
piston stroke 96 mm,
total swept volume 2,44 litre,
weight 69 kg (depending on version),
take−off power (version MIIIB) 55 kW/75 HP
at 2 760 rpm,
max. continuous power 51 kW/69 HP
at 2 600 rpm.
D
T
T
F
T
F
A
A
R
R
D
D
T
T
F
F
F
A
A
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R
D
D
Parma − Technik, s.r.o.,
Uherskobrodská 962,
763 26 Luhačovice, Czech Republic
www.parmatechnik.cz
e−mail: [email protected]
PBS Velká Bíteš, a.s.
TJ 20
Newly developed small model aircraft turbine
engine is predetermined for professional model
aircraft application. It consists of a single-stage
radial compressor, radial and axial diffuser,
annular combustion chamber and single-stage
axial turbine. It reaches up to 220 N thrust with
the weight less than 2 kg. The engine is controlled by a digital electronic system. Starting is
electrical, as well as the fuel pump.
Engine length
outside diameter
weight (dry)
max. thrust
309 mm,
121 mm,
1,95 kg,
220 N.
PBS Velká Bíteš, a.s.,
Vlkovská 279, 595 12 Velká Bíteš,
Czech Republic
www.pbsvb.cz
e-mail: [email protected]
tel: +420 566 822 304
PBS Velká Bíteš, a.s.
TJ 100
This small turbojet engine has been developed for light air vehicles, such as light and
ultralight sports planes, sailplanes equipped with auxiliary engine, piloted vehicles of
experimental class and various unmanned
air vehicles. TJ 100 is completely newly developed driving unit with excellent weight/thrust
ratio. In the category of small turbojet engines
TJ 100 with its thrust ranks among the best
in the world.
Engine length
outside diameter
weight (dry)
max. thrust
625 mm,
272 mm,
20,6 kg,
1200 N.
PBS Velká Bíteš, a.s.,
Vlkovská 279, 595 12 Velká Bíteš,
Czech Republic
www.pbsvb.cz
e-mail: [email protected]
tel: +420 566 822 304
31
ENGINES
D
A
R
T
F
PBS Velká Bíteš, a.s.
TP 100
T
F
The basis of TP 100 is the proven engine TJ
100, which fulfils here the functions of the
gas generator, drives the free turbine and a
three-bladed propeller with constant speed
(via a gearbox). The system is designed for
use in both push and tractor configuration
depending on its mounting on the air vehicle. This engine is intended for the category
of ultralight both piloted and pilotless air
vehicles (UAV).
A
R
Dimensions
870 x 330 x 382 mm,
weight (dry)
55 kg,
output shaft power
180 kW,
propeller speed 2158 rpm,
Thrust with Avia 723 propeller 5394 N.
D
T
F
T
F
A
A
R
R
D
D
D
PBS Velká Bíteš, a.s.,
Vlkovská 279, 595 12 Velká Bíteš,
Czech Republic
www.pbsvb.cz e-mail: [email protected]
tel: +420 566 822 304
PBS Velká Bíteš, a.s.
TS 100
TS 100 is a modified variant of the turboprop engine TP 100. The gearbox is
modified for the operation with propeller
blades. The engine is suitable as a driving
unit of an ultralight helicopter.
Dimensions and weight are the same as
for TP 100.
Output shaft speed 6000 rpm
PBS Velká Bíteš, a.s.,
Vlkovská 279,
595 12 Velká Bíteš,
Czech Republic
www.pbsvb.cz
e-mail: [email protected]
tel: +420 566 822 304
Trefil Engine, s.r.o.
D
32
A
R
T
F
Alfa T−422
This horizontally−opposed four−cylinder
aircooled
fuel−injected
single−OHC
direct−drive engine uses an electronic
ignition and injection control unit by
Ignitech.
F
A
Swept volume 2 183 cc,
bore 95 mm, stroke 77 mm,
compression ratio 1:9,3,
max. take−off power 63 kW /85 HP
at 2900 rpm,
dry weight 74 kg,
equipped weight 81 kg,
max. permitted rpm 3600,
time to major overhaul 2500 h
R
D
Trefil Engine, s.r.o.,
Suterova 2013,
709 00 Ostrava − M. Hory,
Czech Republic
www.trefil.net
e−mail: trefil@trefil−engine.cz
T
CZECH AVIATION 2012
D
A
R
T
F
Verner Motor
JCV−360
T
F
A brand−new twin−cylinder water−cooled
four−stroke petrol aero engine. Four valves
per cylinder. The engine is designed
to power paraglider trikes, ultralight
single−seaters and for other applications.
A
R
Length width height weight operational rpm power output 58 cm,
34 cm,
36 cm,
26 kg,
5500 − 6500
28 kW / 38 HP
D
T
T
F
T
F
A
A
R
R
D
D
T
T
F
F
F
A
A
R
R
D
D
Verner Motor,
Vikýřovice 562,
788 13 Šumperk,
Czech Republic
www. vernermotor.com
e−mail: [email protected]
Verner Motor
VM 144H
Verner VM 144H is a new engine designed
for light helicopters, microlights and light
sport aircraft. The engine is equipped with
electronic fuel injection and air cooling
system with internal fan.
Length 490 mm,
width 736 mm,
height 350 mm,
weight 61 kg,
operational rpm 3900 − 4700
power output 54 kW (74 HP) / 4700 rpm.
Verner Motor
Vikýřovice 562,
788 13 Šumperk,
Czech Republic
www. vernermotor.com
e−mail: [email protected]
Verner Motor
VM 133MK
Light aircraft engine for microlight and
light (experimental) sport aircraft. The
Verner VM 133MK engine is a new model
developed by Verner Motor Company
based on the experience gained from the
production of the first model Verner 1400.
Length 617 mm,
width 736 mm,
height 456 mm,
weight 61 kg,
operational rpm 4000 − 4800,
power output 63 kW (84 HP) / 5500 rpm.
Verner Motor,
Vikýřovice 562,
788 13 Šumperk,
Czech Republic
www. vernermotor.com
e−mail: [email protected]
33