Let L-40 Meta-Sokol
1956
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Let L-40 Meta-Sokol

Designed and produced originally by Ceskoslovenske Zavody Automobilove A Letecke, under which heading all post-World War II aviation activity in Czechoslovakia was first combined, production of the L-40 Meta-Sokol was continued by Letecky Narodni Podnik (Let) after this manufacturer was established at Kunovice in the mid-1950s. A four-seat cabin monoplane of all-metal construction, suitable for training or sporting use, the Let L-40 was of low-wing configuration and incorporated unusual 'reversed-tricycle' landing gear. All three units retracted, but the short-wheel-base tailwheel unit was mounted beneath the cabin so that the fuselage was almost horizontal when the aircraft was on the ground. As first flown in 1956 the L-40 was powered by a 104kW Walther M 332 inline engine, but series aircraft were available with either this engine or a 78kW Walther Minor 4-III. When production ended in 1961, 200 L-40s had been built.


Specification 
 ENGINE1 x Walther M 332 inline engine, 104kW
 WEIGHTS
    Take-off weight935 kg2061 lb
 DIMENSIONS
    Wingspan10.05 m33 ft 12 in
 PERFORMANCE
    Max. speed240 km/h149 mph

Comments 
Peter V. Hartmann, xdh(@)xdh.ca, 10.11.2008

Small correction - L-40 Meta-Sokol was designed and produced by a Czech company called "Orlican", and not by LET.

Helmut Grünbergs, gruenbergs-documentarY(@)t-online.de, 24.04.2007

Dear Sirs, have your for this all Model Service Bulletins, Letters...? I need this for safety flight and maintenance .
Best Regards, helmut Grünbergs

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