"},"prime units?":{"wt":"met"},"crew":{"wt":"two"},"capacity":{"wt":""},"length m":{"wt":""},"length ft":{"wt":""},"length in":{"wt":""},"length note":{"wt":""},"span m":{"wt":"12.6"},"span note":{"wt":""},"height m":{"wt":""},"height ft":{"wt":""},"height in":{"wt":""},"height note":{"wt":""},"wing area sqm":{"wt":"21"},"wing area note":{"wt":""},"aspect ratio":{"wt":""},"airfoil":{"wt":""},"empty weight kg":{"wt":"200"},"empty weight lb":{"wt":""},"empty weight note":{"wt":"(less than)"},"gross weight kg":{"wt":""},"gross weight lb":{"wt":""},"gross weight note":{"wt":""},"max takeoff weight kg":{"wt":""},"max takeoff weight lb":{"wt":""},"max takeoff weight note":{"wt":""},"fuel capacity":{"wt":""},"more general":{"wt":""},"eng1 number":{"wt":"1"},"eng1 name":{"wt":"[[Harley-Davidson]]"},"eng1 type":{"wt":"two cylinder, geared down 3:1"},"eng1 kw":{"wt":""},"eng1 hp":{"wt":"12.5"},"eng1 note":{"wt":". Removable for use as glider"},"power original":{"wt":""},"prop blade number":{"wt":"2"},"prop name":{"wt":""},"prop dia m":{"wt":""},"prop dia ft":{"wt":""},"prop dia in":{"wt":""},"prop dia note":{"wt":""},"perfhide":{"wt":"Y"},"max speed kmh":{"wt":""},"max speed mph":{"wt":""},"max speed kts":{"wt":""},"max speed note":{"wt":""},"cruise speed kmh":{"wt":""},"cruise speed mph":{"wt":""},"cruise speed kts":{"wt":""},"cruise speed note":{"wt":""},"stall speed kmh":{"wt":""},"stall speed mph":{"wt":""},"stall speed kts":{"wt":""},"stall speed note":{"wt":""},"never exceed speed kmh":{"wt":""},"never exceed speed mph":{"wt":""},"never exceed speed kts":{"wt":""},"never exceed speed note":{"wt":""},"minimum control speed kmh":{"wt":""},"minimum control speed mph":{"wt":""},"minimum control speed kts":{"wt":""},"minimum control speed note":{"wt":""},"range km":{"wt":""},"range miles":{"wt":""},"range nmi":{"wt":""},"range note":{"wt":""},"endurance":{"wt":""},"ceiling m":{"wt":""},"ceiling ft":{"wt":""},"ceiling note":{"wt":""},"g limits":{"wt":""},"roll rate":{"wt":""},"glide ratio":{"wt":""},"climb rate ms":{"wt":""},"climb rate ftmin":{"wt":""},"climb rate note":{"wt":""},"time to altitude":{"wt":""},"lift to drag":{"wt":""},"wing loading kg/m2":{"wt":""},"wing loading lb/sqft":{"wt":""},"wing loading note":{"wt":""},"power/mass":{"wt":""},"thrust/weight":{"wt":""},"more performance":{"wt":""}},"i":0}}]}" id="mwcA">Data from Deutsches Museum Arkiv [2]
General characteristics
The Klemm Leichtflugzeugbau GmbH was a German aircraft manufacturer noteworthy for sports and touring planes of the 1930s.
A motor glider is a fixed-wing aircraft that can be flown with or without engine power. The FAI Gliding Commission Sporting Code definition is: a fixed-wing aerodyne equipped with a means of propulsion (MoP), capable of sustained soaring flight without thrust from the means of propulsion. In the US, a powered glider may be certificated for up to two occupants, up to 850 kg maximum weight, and with a maximum ratio of weight to wing span squared of 3 kg/m2. Similar requirements exist in European JAA/EASA regulations, at a maximum weight of 750 kg.
The Bristol Gordon England biplanes were a series of early British military biplane aircraft designed by Gordon England for the Bristol Aeroplane Company that first flew in 1912. Designed for easy ground transport, the aircraft could be quickly disassembled.
Klemm L 25, later Klemm Kl 25 was a successful German light leisure, sports and training monoplane aircraft, developed in 1928. More than 600 aircraft were built, and manufacturing licenses were sold to the United Kingdom and the United States.
The RAE Hurricane was a single-seat, single-engined light monoplane designed and built by the Aero Club of the Royal Aircraft Establishment for the 1923 Lympne Motor Glider Competition. It was underpowered with an unreliable engine. Re-engined, it flew in many races, with first place in the 1926 Grosvenor Challenge Cup its greatest success.
The Farman FF 65 Sport was a French built light biplane, with a single engine and tandem seats, intended for sport and touring. First flown in 1919, it achieved modest sales at home and abroad in the early 1920s. Two unusual modifications produced a biplane glider and a low aspect ratio parasol wing machine.
The Carley C.12 was a small Dutch single seat sporting monoplane from the 1920s. There were several developments but only small numbers were produced.
The LFG Roland Pfeilflieger, (Arrow-flyer), was a German swept wing, single engine, two seat biplane built in Germany in 1914. It made one distinguished long duration flight and served in colonial German South-West Africa.
The Albatros L.71 was a two-seat, single pusher engined biplane built in Germany in the 1920s.
The Daimler L20, later known as the Klemm-Daimler L20, was one of the first light aircraft to be built in significant numbers. A two-seater with an engine of only 20 hp (15 kW), it demonstrated the ability of a small aircraft to cope with flights over the Alps in winter and to make transcontinental journeys of over 36,000 km.
The Daimler L21 or Daimler-Klemm L21 was a light twin engined, single seat, parasol winged sports aircraft built in Germany. It was the winner in the lowest powered class of the Round Germany Flight contest of 1925.
The Potez VIII was a French training aircraft which first flew in 1920. Originally it had a very unusual vertical inline engine and a four-wheeled undercarriage, though the production version was more conventional.
The Caudron C.180 was an all-metal, three-engine French ten-seat passenger aircraft, flown about 1930. Only one was built.
The Caudron C.39 was a French three-engined biplane with a cabin for six passengers when the aircraft was equipped as a landplane or four passengers when on floats. It was flown with some success in competitions in 1920 and 1921.
The Avia 50-MP was a French motor glider based on that of the Avia XV-A training glider. First flown in 1934, it was intended to introduce pilots to motor-gliders.
The Handasyde H.2 was a six seat airliner built in the UK in the early 1920s. Only one was completed.
The Udet U 7 Kolibri (Hummingbird) was a single engine, single seat, parasol wing light aircraft, designed and built in Germany in the mid-1920s. Though they had some competition success and set an unofficial lightplane duration record, only two were produced.
The Działowski D.K.D.1 was the first powered aircraft designed by Stanislaw Działowski. It was a low-power high-wing monoplane with a cabin for one passenger. After attending an aviation exhibition in Warsaw in 1927 it was badly damaged when the engine failed as it left and it did not fly again.
The Nowotny N-y 4bis was a tandem two-seat light aircraft, built in Poland, as a step towards a very light, low-powered training aircraft for flying clubs. Its designer was killed in a glider soon after the first flight of his trainer and its development was abandoned.
The Alcor Duo-4 was a high wing cabin aircraft, unusually powered by a pair of four cylinder straight engines mounted horizontally either side of the nose. After an accident it was rebuilt with six cylinder engines, becoming the Alcor Duo-6. The name Alcor derived from Allan Lockheed Corporation.