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