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Maintenance Manual V001
FRECCIA
1.2. DIMENSIONS
WING
Wing span
Wing chord
Wing surface
Dihedral
AILERONS
Aileron span
Mean chord
Aileron surface
Steering angle (stroke)
FLAPS
Flap span
Mean chord
Flap surface
Flaps positions
FUSELAGE
Total length
Max width
Max height
Frontal surface
Max section surface
Fuselage surface crossed by air flow
TAIL PLANE (HORIZONTAL TAIL)
Wing span
Mean chord
Aspect ratio
Extension
Angle of incidence
Seite 8
8,777 m
1,209 m
10,13 m
2
5°
1,741 m
0,27 m
2
0,47 m
24° ± 1° (up)
12° ± 1° (down)
1,741 m
0,38 m
0,66 m
2
0° / 35° (down)
7,248 m
1,20 m
2,553 m
1,20 m
2
1,00 m
2
14 m
2
2,972 m
0,758 m
2,2 m
2
4,3
+ 1,2
ELEVATOR
Elevator span
Surface
Stroke
TRIM
Width
Chord
Stroke
VERTICAL FIN
Vertical fin span
Minimum chord
Maximum chord
Mean chord
Surface
Extension
RUDDER
Surface
Steering angle
ENGINE
Engine model
Maximum rotational speed of the propeller
Maximum rotational speed of the engine
Propeller
UNDERCARRIAGE
Width of the rear landing gear (undercarriage)
Distance between the turning wheel and the rear
landing gear
Maintenance Manual V001
FRECCIA
2,972 m
0,77 m
2
20° (up)
15° (down)
0,75 m
0,075 m
20°±2° (up)
20°±2° (down)
1,351 m
0,645 m
1,236 m
0,947 m
1,12 m
2
1,4
0,42 m
2
±25° ± 1°
ROTAX 912 ULS
2400/2800 according to the engine model
5800 rpm in 5min / 5600
According to the customer's demand
1,6 m
1,5 m
Seite 9
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