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Kl 105

Klemm · General Aviation · Germany · Interwar (1919–1938)

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The Klemm Kl 105 was a two-seat sport aircraft developed in Germany in 1938. It was a low-wing cantilever monoplane of conventional design with fixed, tailskid undercarriage, and side-by-side seating for two within an enclosed cockpit. Construction throughout was of wood, with the fuselage built using a new semi-monocoque technique which Klemm patented. Plans to produce the design in series were abandoned with the outbreak of the Second World War.

Specifications

Category
Fixed Wing
Sub-Category
General Aviation
Domain
Civil
Era
Interwar (1919–1938)
Country
Germany
Manufacturer
Klemm
Service Entry
1938
Engine
Zündapp Z 9
Thrust / Power
50 hp (37 kW)
Length (ft)
24
Wingspan (ft)
35
Empty Weight (lb)
750
MTOW (lb)
1230
Service Ceiling (ft)
9800
Range (mi)
310
Max Speed (mph)
90