type of aircraft
Klemm Kl 105
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.
Summary from Wikipedia licensed under CC BY-SA.
- Manufacturer
- Klemm
- Country of origin
- Germany
Specifications
- Cruise speed
- 78 kt
- Max speed
- 78 kt
- Range
- 270 nm
- Service ceiling
- 9,800 ft
- Rate of climb
- 350 ft/min
- Max takeoff weight
- 1,230 lb
- Empty weight
- 750 lb
- Powerplant
- Zündapp Z 9
- Engines
- 1
- Seats
- 2
- Length
- 24.1 ft
- Wingspan
- 35.8 ft
- Height
- 6.6 ft
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.