Pro.Mecc Freccia, Руководство по обслуживанию

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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