Dyn'Aéro
S.A. 19, rue de l'Aviation 21121 DAROIS
(33) 03 80 35 60 62 Fax: (33) 03 80 35 60 63
28/02/2006
Q EX NO 07 00
MCR 4S FLIGHT MANUAL
[MAJ
28/02/06]
Page N°10 /
39
NOTE:
Attracts the attention to a condition which although not particularly related to the flight safety is
important or unusual.
2.4. S
PECIFICATIONS
Kit aircraft of the type :
Dyn'Aéro
MCR 4S
Cantilever low-mounted wing.
Carbon structure and wing skin with control surface skins made in light alloy.
Engine and Propeller
Span
8.66
m
Wing surface
8.15
m²
Aspect ratio
9.2
Cabin width
1.17
m
Fuel capacity
2 x 60
l
Overall Length
6.72
m
Height
1.95
m
2.5. C
ONTROL SURFACE DEFLECTION
Ailerons :
- 20°
(
±
1)
trailing edge upwards
+10°
(
±
1)
trailing edge downwards
Flaps :
0-30°
(+0-1)
Rudder :
20°
(-0+5)
in both directions (left and right)
Tailplane :
- 10°
(+0-2)
trailing edge upwards
+3.5°
(-0+1)
trailing edge downwards