ULL Classic Skylane MH−46 Eclipse UL-LSA AIRCRAFT

ULL Classic Skylane MH−46 Eclipse UL-LSA AIRCRAFT

UL-LSA AIRCRAFT
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.)
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 Republic
www.aerosette.eu
e−mail: info@aerosette.eu
ULL Classic
Classic - 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 kg
cruising speed 180 -220 km/h
Aerospool CZ, s.r.o.
Hlavní 439
687 25 Hluk
Czech Republic
www.aerospool.cz
e-mail: info@aerospool.cz
Skylane
A two-seat side-by-side braced high-wing
ultralight monoplane of mixed, mainly
composite structure. Fixed tricycle undercarriage. 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 Republic
www.airlony.cz
e−mail: airlony@airlony.cz
CZECH AVIATION 2011
Highlander
A 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 Republic
www.airlony.cz
e−mail: airlony@airlony.cz
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 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 Republic
www.atecaircraft.eu
e−mail: sales@atecaircraft.eu
Atec 212 Solo
A single−seat ultralight airplane of composite structure. Fixed tailwheel undercarriage. Stressed for +6/−3 g. Powered by
Rotax 582UL DCDI or 912UL. (So far 7
machines built.)
Span 7,50 m, length 5,26 m,
wing area 7,30 m2,
empty weight 200 kg,
max. level speed VH 245 km/h.
Atec, v.o.s.,
Opolanská 350,
289 07 Libice nad Cidlinou,
Czech Republic
www.atecaircraft.eu
e−mail: sales@atecaircraft.eu
UL-LSA AIRCRAFT
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. (215
units built so far.)
Span 9,40 m, length 6,20 m,
wing area 10,30 m2,
empty weight 275 kg,
max. level speed VH 245 km/h.
Atec, v.o.s.,
Opolanská 350,
289 07 Libice nad Cidlinou,
Czech Republic
www.atecaircraft.eu
e−mail: sales@atecaircraft.eu
VL−3 Sprint
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.,
Aveko Aircraft, a.s.,
Toulovcovo nám. 1163,
570 01 Litomyšl,
Czech Republic
www. vanessaair.cz
e− mail: vanessaair@lit.cz
Lipová 22,
602 00 Brno,
Czech Republic
www.VL−3.com
e−mail: VL−3@aveko.com
NG 5
UL, ELSA, LSA, RG – all metal two seater 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 1224
686 05 Uherské Hradiště
Czech Republic
www.brmaero.com
info@brmaero.com
CZECH AVIATION 2011
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 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 1177/212
Kunovice 686 04, Czech Republic
Phone: + 420 576 514 032
Fax: + 420 576 519 394
e-mail: office@czechsportaircraft.com
www.czechsportaircraft.com
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 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 1177/212
Kunovice 686 04,Czech Republic
Phone: + 420 576 514 032
Fax: + 420 576 519 394
e-mail: office@czechsportaircraft.com
www.czechsportaircraft.com
Alto
An 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 Republic
www.directfly.cz, www.flyshop.cz
e−mail: info@directfly.cz
UL-LSA AIRCRAFT
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, www.flyshop.cz
e−mail: info@directfly.cz
DV−1 Skylark
A 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 Republic
www.dovaaircraft.cz
e−mail: centrum@dovaas.cz
UFM−13 Lambada
A side−by−side two−seat, mid−wing ultralight of composite structure. Fixed tricycle or tailwheel undercarriage. Powered
by Rotax 912UL, 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.
(So far 135 aircraft in the UFM−11 −13 versions 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.
Production division:
Company headquarters:
Distar − Air,
Distar CZ, a.s.,
U Letiště 1381,
562 01 Ústí nad Orlicí
Czech Republic
10
1. máje 228,
504 01 Nový Bydžov,
Czech Republic
e−mail: info@distar.cz
e−mail: air@distar.cz
www.distar.cz
CZECH AVIATION 2011
Samba XXL
A low−wing, composite side−by−side
two−seat ultralight monoplane. Fixed tricycle undercarriage. Powered by Rotax
912UL or ULS engines, with fixed or
variable−pitch propeller. (93 aircraft have
been built so far).
Span 10,00 m, length 6,00 m,
wing area 8,90 m2,
empty weight 260 kg,
cruising speed 220 km/h.
Production division:
Company headquarters:
Distar − Air,
Distar CZ, a.s.,
U Letiště 1381,
562 01 Ústí nad Orlicí
Czech Republic
1. máje 228,
504 01 Nový Bydžov,
Czech Republic
e−mail: info@distar.cz
e−mail: air@distar.cz
www.distar.cz
SR−01 Magic
Tandem two−seat low−wing all−metal
monoplane with tricycle fixed undercarriage. Powered by Rotax 912ULS, turning 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 Republic
www.aeromagic.cz
e−mail: vlasta.kriz@centrum.cz
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 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.com
e−mail: marketing@evektor.cz
11
UL-LSA AIRCRAFT
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 engine,
with fixed or variable pich propeller. Fixed
tricycle undercarriage. Altogether over
1000 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: marketing@evektor.cz
SportStar RTC
An all metal side−by−side two−seat training 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.
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: marketing@evektor.cz
Harmony / Harmony LSA
A side−by−side two−seat cantilever lowwing advanced UL / LSA aircraft of all
metal structure. Fixed tricycle undercarriage. Powered by Rotax 912UL or ULS
engines, with fixed of variable pitch propeller. The Harmony has curved wing,
120 l wing tanks providing 1300 km range
and outstanding cockpit spaciousness.
Span 8,68 m, length 6,11 m,
wing area 9,84 m2,
weight 295 kg,
cruising speed 210 − 245 km/h.
Evektor−Aerotechnik, a.s.,
Letecká 1384,
686 04 Kunovice,
Czech Republic
www.evektoraircraft.com
e−mail: marketing@evektor.cz
12
CZECH AVIATION 2011
Evolution E80 / E100
A 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:
tomas.sedlacek@fascination.aero
Fascination F80 / F100
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), 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:
tomas.sedlacek@fascination.aero
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
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 speed180 − 230 km/h.
Flying Machines, s.r.o.,
Rasošky 132,
55221 Rasošky,
Czech Republic
www.flyingmachines.cz
e−mail: info@flyingmachines.cz
13
UL-LSA AIRCRAFT
FM−301 Stream
FM-301 Stream is an all composite two seater microlight trike of frameless load bearing
construction. The aerodynamic shape of
the machine makes it quite easy and comfortable 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 instrument 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 Republic
www.flyingmachines.cz
e−mail: info@flyingmachines.cz
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
co−vered in Ceconite fabric.
Powered by a single−cylinder Flyengine
F200 two−stroke of 19 kW/26 hp.
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.
Tr. E. Beneše 1561
50012 Hradec Kralove
Czech Republic
www.IvanovAero.cz
e−mail: zjviera@email.cz
Skyleader 100
The Skyleader 100 is an all metal one-seat,
low wing, ultralight aircraft with a rectangular 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.
Span 6,9 m, length 5,6 m,
wing area 8,82 m2,
empty weight 210 kg,
cruising speed 160 km/h.
Jihlavan Airplanes, s.r.o.
Znojemská 826/64
586 01 Jihlava
Czech Republic
e-mail: market@skyleader.aero
www.skyleader.aero
14
CZECH AVIATION 2011
Skyleader 200 / 500
The Skyleader 200 is an all metal twoseat, low wing, UL/LSA aircraft with a trapezoidal 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 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 kg
cruising speed 215 km/h.
Jihlavan Airplanes, s.r.o.
Znojemská 826/64,
586 01 Jihlava,
Czech Republic
www.skyleader.aero
Skyleader 600
The Skyleader 600 is an all metal twoseat, low wing, constructed aircraft with
a trapezoidal 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 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.
Jihlavan Airplanes, s.r.o.
Znojemská 826/64,
586 01 Jihlava,
Czech Republic
www.skyleader.aero
Skyleader GP ONE
The Skyleader GP ONE is carbon-composite two-seat, high wing ultralight aircraft 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.
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
15
UL-LSA AIRCRAFT
Jora
A 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 propeller 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.cz
e−mail: joraul@quick.cz
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: info@kubicekaircraft.cz
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 could
be powered by engines in the range of
23-50 HP. Also suitable for amateur construction. (30 kit-built aircraft have been
produced so far.)
Span 6 m, lenght 4,3 m
Wing area 6 m2
empty weight 120 kg
gross weight 240 kg
max. speed in horizontal flight 190 km/h.
Spacek s.r.o.
Lesní 25
695 01 Hodonín
Czech republic
www.sdplanes.com
e-mail:info@sdplanes.com
16
CZECH AVIATION 2011
Shark
A tandem two-seat high performance ultralight/LSA/ELA low wing with all-composite,
mostly carbon airframe. Retractable undercarriage 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 prototypes 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 835
687 25 Hluk
Czech Republic
www.shark.aero
e-mail: shark@shark.aero
TL-2000 Sting S4
New 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 aircraft made from carbon fiber. Powered by
Rotax 912UL or 912ULS, turning a groundadjustable 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.
TL-ultralight s.r.o.
Letiště − budova č. 84
503 41 Hradec Králové, Czech Republic
www.tl-ultralight.cz
e-mail: sales@tl-ultralight.cz
TL-3000 Sirius
A 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. 84
503 41 Hradec Králové, Czech Republic
www.tl-ultralight.cz
e-mail: sales@tl-ultralight.cz
17
UL-LSA AIRCRAFT
TL-2000 Sting
A side-by-side two-seat cantilever lowwing light sport aircraft of composite construction 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 manufactured).
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.
TL-ultralight s.r.o.
Letiště − budova č. 84
503 41 Hradec Králové, Czech Republic
www.tl-ultralight.cz
e-mail: sales@tl-ultralight.cz
Viper SD-4
Viper SD – 4 is an aerodynamically controlled, 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 control 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 467
250 64 Měšice
Czech Republic
www.tomarkaero.com
e-mail: tomarkaero@tomarkaero.com
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
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 letadel
Újezd u Uničova 87,
783 96,
Czech Republic
www.podesva−air.com
e−mail:t.podesva@cmail.cz
18
CZECH AVIATION 2011
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:t.podesva@cmail.cz
Trener UL
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 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:t.podesva@cmail.cz
Savage
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
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 Republic
www.zlinaero.com
19
UL-LSA AIRCRAFT
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−bla−ded, ground−adjustable compo­
site 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: v.rajchl@volny.cz
Tomi−Cross 5 Sport
Tandem 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. Řehák
Budovatelů 301,
533 13 Řečany nad Labem,
Czech Republic
www.rogalo.info
aviatik.r@seznam.cz
Sonet
An all composite, side−by−side two−seat,
cantilever low−wing ultralight. It has excellent 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 Republic
www.airsport.cz
e−mail: info@gramex.cz
20
CZECH AVIATION 2011
Sonata
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.
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.
Gramex, s.r.o.
Zbraslavice 399,
285 21 Zbraslavice,
Czech Republic
www.airsport.cz
e−mail: info@gramex.cz
Song
A single seat, carbon fibre composite aircraft 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.
Gramex, s.r.o.
Zbraslavice 399,
285 21 Zbraslavice,
Czech Republic
www.airsport.cz
e−mail: info@gramex.cz
U−15 Phoenix
U−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 removable 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 Orlicí
Czech Republic
www. phoenixair.cz
e−mail: info@phoenixair.cz
21
UL-LSA AIRCRAFT / GLIDERS
Banjo MH
A single−seat braced high−wing ultralight
of mixed wood/glassfibre structure, powered by Hirth F33B. Retractable wooden 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.
ProFe
Leštinská 811,
549 01 Nové Město nad Metují,
Czech Republic
www.profe.cz
e−mail: info@profe.cz
Duo Banjo
A two−seat braced shoulder−wing ultralight of mixed wood/glassfibre structure,
powered by Rotax 447. Retractable wooden two−bladed 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: info@profe.cz
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 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. složka
Zahradní 995,
594 01 Velké Meziříčí,
Czech Republic
www.testandfly.cz
e−mail: comp-let@complet.sk
22
CZECH AVIATION 2011
TST−10MC Atlas
A single-seat ultralight powered glider
of composite structure. The single-wheel
retractable undercarriage and automatic connection of controls. Powered by
retractable Rotax 447 unit and two-bladed
fixed propeller. BRS and optimized winglets 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
Test, Comp−Let, s.r.o., org. složka
Zahradní 995,
594 01 Velké Meziříčí,
Czech Republic
www.testandfly.cz
e−mail: comp-let@complet.sk
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-bladed fixed
propeller. BRS and optimized winglets
option. (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: comp-let@complet.sk
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 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 Holešov
Očadlíkova 36
Czech Republic
e−mail: obartonik@volny.cz
23
GLIDERS / AIRCRAFT
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 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 Republic
www.shvl.cz
e−mail: info@shvl.cz
Discus CS
A 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 Republic
www.shvl.cz
e−mail: info@shvl.cz
HPH−304S/SJ Shark
PHP-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 mainwheel 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 Republic
www.hph.cz
e−mail: hph@hph.cz
24
CZECH AVIATION 2011
HPH−304MS Shark
A 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 Republic
www.hph.cz
e−mail: hph@hph.cz
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 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 Republic
www.hph.cz
e−mail: hph@hph.cz
M1 SpeedCruiser
The 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 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,
MTOW 1 170 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: hpai@mbox.cz
25
AIRCRAFT
SM−92TE Silver Fox
SM−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 propeller. 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 5
Subsidiary: International Airport
Hradec Králové (LKHK)
www.orbisavia.cz
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−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.com
e−mail: marketing@evektor.cz
EV−55 Outback
The EV−55 Outback is the new generation twin engine utility turboprop airplane 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.com
e−mail: marketing@evektor.cz
26
CZECH AVIATION 2011
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,
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 Republic
www.let.cz
e-mail: let@let.cz
Z 242 L
The Zlin Z 242 L is a sport and aerobatic
two-seater brand Zlin aircraft powered
by single engine Lycoming AEIO-360A1B6 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.
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
info@zlinaircraft.eu
Z 143 LSi
The 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, MTV9-B/195-45 propeller, of 855 kg/1885 lbs
weight. Simple handling, all metal structure of fuselage.
Span 10,14 m, length 7,58 m,
wing area 14,77 m2,
empty weight 855 kg,
cruising speed 243 km/h.
Zlin Aircraft a.s.
Letiště 1578
76581 Otrokovice
Czech Republic
www.zlinaircraft.eu
info@zlinaircraft.eu
27