#### MechAeroAuto

##### Well-Known Member

http://www.rsafrance.com/index.php/construire/liasses/chouchenn

from Googlé Translate

The '' Chouchenn '' is a small two-seater airplane side by side with 284 Kg of empty mass, 8.5 m of wingspan that stalls at full load at less than 70 km / h all released. Motorized with a Jabiru 2200 it cruises at 218 Km / h at 75% for a consumption of 14.5 L / h. Already presented in the Notebook of the RSA n ° 272 in 2011 it has today 425 h the counter and soon sees its 2nd visit of airworthiness arrives

[h=3]Technical characteristics[/h]

Fuselage

Length: 5.645 m ht

Width: 1.10 m to the master bau

SM: 8.1 m²

Stabilizer H

Wingspan: 2.5 m

String: 0.6 m

Surface: 1.5 m2

Profile: NACA 12 modified

SM: 3 m²

Empennage V

Profile: Modified NACA

Total surface area: 0.738 m2

Surface direction: 0.312 m2

(41%)

SM: 1.37 m²

Motorization

Jabiru 2200A

P: 85 HP / 3300T / mn Consumption

: 15 l / h

Autonomy: 4h

Propellers: Woodpecker 1.47m, step: 1.1m

Weight

: Empty Weight: 284 Kg

A full load: 498 Kg

Fuel: 50 Kg (70 l)

Centering17 to 36%

Wing

Wingspan: 8.5 m

NACA Profile 23015 Rope: 1 m

Elongation: 8.5

Surface: 8.5 m2

Dierdre: 3 °

Twist: -1 °

Ailerons: 1.2m., Rope 256 mm

Shutters: single slot 2.3 m,

rope: 256 mm,

deflection : 0 °, 13 °, 35 °

SM: 17 m²

Speed

VNE: 270 km / h,

V cruising: 218 km / h / 75%

V stall in heald with

maximum mass <90 km / h

V stall at 13 ° of flaps and mass

max <78Km / h

V stall at 35 ° Flaps and mass

max <70 Km / h

V rotation 95 Km / h