


So you wanna fly this real smallest aircraft in the world? Michael Colomban Cri cri - Cricket Aircraft - Cri cri plan - Cricri construction - Drawing Plan
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Noted French pilot Nicolas Charmont has installed 2 AMT Olympus turbines in his Cri Cri together with AMT on-board automatic start-up units and individual EDT's. The Cri Cri weighs 170 Kg, and should have enhanced performance withover 36 Kg of thrust available. The Cri Cri has made his maiden flight in the weekeind of 7-8 March. More info :http://www.amtjets.com/ |
| Formation flight with that intriguing airplane, Michel Colomban's Cricri MC15. Known to be the smallest twin-engined airplane in the world (4.90m wingspan, 72kg empty weight, 2x15HP), it still has a 190km/h cruise speed and is capable of executing all the basic aerobatic maneuvers.
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Min speed: | 39 kt | 45 mph | 72 kmh |
Cruise speed: | 108 kt | 124 mph | 200 kmh |
Vne: | 159 kt | 183 mph | 295 kmh |
MC-10 | Cri-Cri | MC-12 Cricket MC-12 Cricket |
Wingspan | 5 m 5 m | 4,9 m 4,9 m |
Captain | 3,9 m 3,9 m | |
Wing area | 3,1 m2 3,1 m2 | |
Re-air | 63 kg 63 kg | 75 kg 75 kg |
Take-off weight | 170 kg 170 kg | |
Wing load | 55 kg/m2 55 kg/m2 | |
Engine Model | 2x 9PS 2x 9PS | 2x 15PS 2x 15PS |
Overload factor | +9G, -4,5G +9 G, -4,5 G | +9G, -4,5G +9 G, -4,5 G |
Maximum speed | 200 km/h 200 km / h | 250 km/h 250 km / h |
Cruising speed | 170 km/h 170 km / h | 185 km/h 185 km / h |
Rate of climb | 3 m/s 3 m / s | 6 m/s 6 m / s |
Roll away | 150 m 150 m | 120 m 120 m |
Ceiling | 5500米 5500 m | |
Voyage | 750 km 750 km | 500 km 500 km |
The Cri-Cri is a popular homebuilt design developed in France by engineer and pilot Michel Colomban. Colomban became fascinated by small aircraft and hoped to create a tiny and economical plane with good performance and aerobatic capabilities. His goal was a very simple and lightweight construction using no more than a 20-hp engine powering an airframe carrying a 172 lb (78 kg) pilot and 22 lb (10 kg) of fuel. Colomban's initial study in the late 1950s suggested that a single seat aircraft with a maximum takeoff weight of 395 lb (180 kg) and a wing area of 43 ft² (4 m²) was feasible.
Over a decade later, Colomban returned to his pet project but was able to make several improvements due to advances in technology. He incorporated new more efficient low-drag airfoils, composite parts, and thinner sheet metal for the wing skin to reduce weight and wing area to just 33 ft² (3.1 m²). The new aircraft also adopted twin 8-hp Stihl chain-saw engines, like those used aboard ultralights, in place of the planned single 20-hp engine. The change not only made the aircraft lighter but also improved the efficiency of each engine's propeller. Construction of the first example took about 1,500 hours, and several structural load tests were conducted to prove its advanced design elements were safe.