Klemm Kl 105
The Klemm Kl 105 was a civilian sports and touring aircraft in the light Klemm GmbH.
Designed in 1938, the aircraft was in the self- developed and patented by Hanns Klemm ( EN 729 100 of 6 November 1936) part shell design. The aircraft was a cantilever low- wing monoplane of all-wooden - part shell construction with rigid unverkleidetem normal chassis. The two-man crew sat side by side in an enclosed cabin. The fracture load factor was 7.2. The engine drove a rigid two-bladed wooden propeller of two meters in diameter. The wings were folding exterior parts, so that the aircraft for parking had a width of only 2.3 meters. It only eleven sample machines were manufactured due to the war.