|
|
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.
| ENGINE | 1 x Walther M 332 inline engine, 104kW |
| WEIGHTS |
| Take-off weight | 935 kg | 2061 lb |
| DIMENSIONS |
| Wingspan | 10.05 m | 33 ft 12 in |
| PERFORMANCE |
| Max. speed | 240 km/h | 149 mph |
| 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 |
|
Do you have any comments about this aircraft ?
|
| |