MechAeroAuto
Well-Known Member
It's a neat looking little plane for those who are interested. I couldn't find an instance of it being discussed here so I thought I would share. I believe it says "bundles" (plans) are available but I don't know how you go about getting them. Anyways, presenting the "Honey Wine".
http://www.rsafrance.com/index.php/construire/liasses/chouchenn
from Googlé Translate
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)
Centering
17 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