Let L-200 Morava

infobox Aircraft
name =L-200 Morava
type =Touring / utility aircraft
manufacturer =Let



caption =L-200A as an air ambulance, at the Polish Aviation Museum
designer =
first flight =9 April 1957
introduced =
retired =
status =In service in private hands
primary user =Czechoslovakia
more users =USSR, Poland
produced =1957-1964
number built =367
unit cost =
variants with their own articles =The Let L-200 Morava is a two-engine touring and light passenger aircraft of the 1960s, designed and produced in Let Kunovice in Czechoslovakia.

Development

The factory Let (from 1957 to 1967 - SPP) in Kunovice manufactured the two-engine touring aircraft Aero Ae 45 under licence from Aero in the 1950s. A newly created in 1955 construction bureau, led by Ladislav Smrček, decided to design its own, more modern five-seat touring aircraft. It was initially decided to use the new 210 hp engines M-337, but since it was not ready, the prototype was fitted with less powerful 160 hp Walter Minor 6-III engines.

The first prototype designated XL-200 (OK-LNA) flew on 9 April 1957, followed by the second prototype (OK-LNB) and another for static trials. The plane had very elegant, slim lines. In the same year, 10 pre-series aircraft L-200 were manufactured. One of them underwent state trials in 1958. The aircraft was successful and ordered into production. One L-200 was converted into a prototype of M-337-powered serial variant L-200A. Changes were minor, mostly new two-blade propellers V-410, cockpit lowered by 43 mm, modified tailfin shape and longer engine nacelles. It was completed in 1959 and shown in the Paris Air Show in July of that year. After being fitted with M-337 engines in autumn 1959, it underwent state trials, completed successfully in July. The first serial plane L-200A was flown in February 1960.

L-200B and C models were not produced. The second production variant was the L-200D, modified according to Russian Aeroflot demands. It was fitted with new three-blade propellers V-506 of a smaller diameter and some minor improvements, such as dust filters. It also received more comprehensive navigation equipment. The prototype (OK-NIA) was converted from the L-200A prototype in 1960 and tested in 1961-1963.

In all, 367 L-200s were builtVaclav Nemecek, "Atlas letadel. Dvoumotorova obchodni letadla", Praha 1987] by 1964, including 3 prototypes and 197 L-200D (eight L-200A and the L-200A prototype were converted to L-200D as well). 5 aircraft were manufactured from parts by Libis in Yugoslavia.

A further development was 6-place L-210 (also known as L-201; registration OK-PHB), converted from one L-200D in 1966, powered with 245 hp M-338 engines, but it was not ordered by the airlines and was not produced.

Operational Service

The pre-series aircraft L-200 were distributed for testing: 5 to the Czechoslovak airline Agrolet (OK-MEA - MEE), 2 to the Czechoslovak Air Force and 2 to the Aeroflot lines in the USSR.

Aeroflot, who used them as air taxis, was the largest single user of Moravas - 68 L-200A and 113 L-200D, final deliveries taking place in 1966. In the 1970s however, the Soviet Union sold or withdrew its aircraft from use, in favour of indigenous designs.

About 100 Moravas were used for civilian purposes in Czechoslovakia by aeroclubs Svazarm (about 50), the airlines Agrolot (from 1969 Slov-Air) and Czechoslovak Airlines (45) and by businesses, such as Škoda. 20 were used by the Czechoslovak Air Force (16 of which L-200A), among others, for training. About 50 were sold to Poland, where they were used mostly as air ambulances and in aeroclubs. Some other countries had smaller fleets of Moravas.

144 L-200A were exported to 15 countries. They were used in Australia, Argentina, Cuba, Hungary, West Germany, Great Britain, Egypt, India, Italy, Poland, South Africa, USSR and Yugoslavia. L-200D were exported to Bulgaria, Cuba, Egypt, France, Hungary, GDR, Great Britain, India, Indonesia, Italy, Poland, Switzerland, Sweden, USSR and Yugoslavia.

Small number of Moravas are still used (as of 2008), mainly in Czech Republic, Slovakia and Poland.

pecifications (L-200A)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
crew=1 pilot
capacity=4
length main=8.61 m
length alt=
span main=12.31 m
span alt=
height main=2.25 m
height alt=
area main=17.28 m²
area alt=
empty weight main=1275 kg
empty weight alt=
loaded weight main=1950 kg
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=
more general=
engine (prop)=Walter M337
type of prop= air-cooled straight engine
number of props=2
power main=210 hp
power alt=154 kW
max speed main=310 km/h
max speed alt=
max speed more=
cruise speed main= 285 km/h
cruise speed alt=
stall speed main=
stall speed alt=
range main=1900 km
range alt=
ceiling main=6100 m
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
power/mass main=
power/mass alt=
more performance=
armament=

ee also

aircontent
related=
similar aircraft=
*Aero Ae 45
*Beechcraft Baron
*Cessna 310
*Beagle B.206
*Piper Aztec
sequence=
lists=
see also=

References

* [http://www.airwar.ru/enc/other/l200.html L-200 Morava] at Ugolok Neba site (in Russian)

External links

* [http://techmag.valka.cz/let_l_l200.htm Photo gallery]
* [http://flyingrevue.cz/index.php/cze/Historie/Historie/Morava-L-200-a-Tatra-T-603-Designove-skvosty-sedesatych-let Flying revue: L-200 Morava and Tatra T-603] at Flying revue magazine (in Czech)