- Zlin Z 142
Infobox Aircraft
name=Zlin 42, 142 and 242 series
caption= Moravan Zlin 242L
type=Sport, personal andtrainer aircraft
manufacturer=Moravan Otrokovice
designer=
first flight=
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variants with their own articles=The Zlin Z 142 is a single-engine two-seat
Czechoslovakia ntrainer aircraft manufactured byMoravan Otrokovice . The Z 142 is the most popular aircraft variant in its aircraft line, with the base model being the Z 42. In contrast to the older Z 40 which had both seats in tandem, all Z 42 series aircraft use side-by-side seating.Design and development
The aircraft were built by Moravan Aviation, founded in
1934 in aviation by Tomas Bata in theCzech Republic .The aircraft fuselage center section is of welded steel tube, covered with
sheet metal andfiberglass panels. The tailcone is of monocoque construction. Theempennage is of sheet metal, and incorporates an all-flying tail. The two-spar wings are of all-metal construction. The tricycle landing gear is fixed, with a steerable nose wheel. The Z 42 is powered by a Walter inverted six-cylinder engine rated at 134 kW (180 hp).The
prototype Z-142 first flew on December 28, 1978.The Zlin Z 142 is a development of the Zlin Z 42 M platform, equipped with a Walter (now LOM) fuel-injected inverted 6 cylinder, supercharged
air-cooled engine rated at 157 kW (210 hp), driving aconstant speed propeller .Designed for aerobatics instruction, it was certified to +6.0 and -4.0 limit maneuvering load factors, and was equipped with full inverted fuel and oil systems permitting extended inverted flight.
In the late 1980s further development work was initiated. The inverted
inline engine was replaced with a four-cylinder horizontally-opposed Lycoming IO-360 engine. This variant is designated the Z 242, and is immediately distinguishable by its relatively widecowling which houses the flat-four engine.Operational history
The Z 42 variants are used for basic and intermediate
VFR flight training , for basicaerobatics training, for night and instrument flight training, and forglider towing.The aircraft were largely used in former
COMECON countries forair club and basicair force training. It was also used by the air forces ofAlgeria ,Mexico andSlovenia . According to theLTTE , it was used in bombing sorties on theSri Lanka n airforce bases in Sri Lanka. [http://news.bbc.co.uk/2.hi/south_asia/6496381.stm] [http:www.theaustralian.news.com.au/story/0,20867,21672616-2703,00.html]There have been wing difficulties resulting in restriction of permitted aerobatic flight time for original aircraft. The factory offers a retrofit package of replacement wings and an AMU-1 fatigue monitoring system, which extends overall airframe life to 5 500 hours, all of which may be aerobatic.
Aerobatics and maneuvers
The Zlin Z 142 was not designed as a fully-aerobatic plane, but it is equipped for inverted flying, and can be used for aerobatic instruction. The following figures are allowed:
* Spins (normal and inverted)
* Loops (except inverted)
*Barrel roll s (except snap rolls)
*Immelmann s
*Wing-over s
*Split-s slide s andTail-slide s
* Inverted flightpecification (Z42)
aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=Fact|date=August 2008
crew=1
capacity=1 passenger or student
payload main=
payload alt=
length main= 7.07 m
length alt=23 ft 2 in
span main=9.11 m
span alt=29 ft 9 in
height main=2.69 m
height alt=8 ft 8 in
area main= 13.152
area alt= 141.55 sq.ft
airfoil=
empty weight main= 600 kg
empty weight alt= 1,323 lb
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 920 kg
max takeoff weight alt= 2,028 lb
more general=
engine (prop)=M137A
type of prop=6 cylinder
number of props=
power main= 134 kW or
power alt=180 hp
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stall speed main=
stall speed alt=
never exceed speed main= 315 km/h
never exceed speed alt= 170 kt IAS
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avionics=Variant specifications
Military Operators
*
*
* - operates 5 Zlin 242Ls
*
*
*
* - operates 9 Zlin 242Ls
*
*
*;Rebels
*Former Military Operators
* - Z-42
* - Z-42References
* [http://www.moravan.cz Moravan official site] . Accessed
October 31 ,2005 .External links
* [http://www.easa.eu.int/doc/Certification/Design_Appro/Aircrafts/TCDS_A_027_Z242_L.pdf European Aviation Safety Agency (EASA) Type-Certificate Data Sheet]
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