Let L-200 Morava

· Let Kunovice · 2 × Avia M 337

Airplanes

Length

8.61 m

Flat Wing Span

12.31 m

Height

2.25 m

Flat Wing Area

17.28 m²

Max Seating

Cruise Speed

256 km/h

Max Speed

290 km/h

Max Ceiling

5700 m

Number of Engines

Aircraft Engine

First Flight

1957-04-09

Number Built

367

Maximum Take-Off Weight

1.95 t (paragliders: kg)

Total Fuel Capacity

420

Maximum Range

1710 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Let L-200 Morava	1.95	420	1710

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
SGP M-222 Flamingo		8.8	11.9		Compare
OMA SUD Skycar		8.92	12	3	Compare
Cessna Skymaster		8.8392	11.5824	5	Compare
Piper PA-34 Seneca		8.72	11.86		Compare
Custer CCW-5	Continental O-470	8.5344	12.4968	4	Compare
Praga E-210	Walter Minor	8.5	12.5	4	Compare

All data (27 fields)

Name: Let L-200 Morava
Manufacturer: Let Kunovice
Description: The Let L-200 Morava is a two-engine touring and light passenger aircraft of the 1960s, designed and produced by Let Kunovice in the Czech Republic.
ICAO Code: L200
First Flight: 1957-04-09
Production End: 1964-01-01
Designer: Milan Křeček
Type: Touring / utility aircraft
Length (m): 8.61
Height (m): 2.25
Cockpit Crew: 1
Max Seating: 4
Max Speed (km/h): 290
Cruise Speed (km/h): 256
Max Ceiling (m): 5700
Rate of Climb (m/s): 6.4008
Capacity Description: 4 passengers
Number Built: 367
Powerplant Description: 2 × Walter M337 air-cooled six-cylinder straight engine, 157 kW (210 hp) each
Primary Users: Czechoslovakia, USSR, Poland
Status: In service with private individuals
Wikipedia Article (URL): en.wikipedia.org/wiki/Let_L-200_Morava
Flat Wing Span (m): 12.31
Flat Wing Area (m²): 17.28
Wake Category: L
Aircraft Engine: Avia M 337
Number of Engines: 2