VENTURA
TM
Ultralight Aircraft
Pilot’s Operating Handbook
VENTURA-POH-ENG
Rev. 00
SERIAL NUMBER:
YY-MM-62-XXXX-Z
FIRST ISSUE:
04/05/2018
REVISION 00:
04/05/2018
NOT CONTROLLED COPY
PAGE:
24/60
2.10. TECHNICAL SPECIFICATIONS
Fuel system
Fuel capacity
2 x 36 lt
Collector tank (Nourice)
6 lt
Lubrication
Type
Engine driven oil pump
Capacity
2.5 lt
Cooling
Type
Air-water-oil
Liquid capacity
3.3/3.5 lt
Electrical system
Battery
Minimum 9 Ah
Generator
250 W
Starting
Electric
Geometric features
Wingspan
9 m
29.5 ft
Height
2.72 m
8.9 ft
Length
7.3 m
23.95 ft
Max fuselage width 1.16 m
3.80 ft
Luggage mass
20 kg (luggage area) +
90+90 kg (rear cabin area)
44 + 200 + 200 lbs
C.G. forward limit
19% MAC
C.G. rear limit
35% MAC
Number of occupants
2
Wing loading (MTOW 450 Kg / 992 lbs)
33 Kg/m
2
6.8 lbs/ft
2
Wing loading (MTOW 600 Kg / 1320 lbs)
44.4 Kg/m
2
9.1 lbs/ft
2
Mean aerodynamic chord (MAC)
1.5 m
4.92 ft
Wing surface
13.5 m
2
145
ft
2
Wing extension
6
Chord ratio
1
Flaperon surface
0.81 m
2
8.72 ft
2
Flaperon span
3.733 m
12.25 ft
Flap angles
0°; 13.5° ± 2°; 27° ± 2°
Ailerons angles (flaps UP)
± 15.5° ± 2°
Horizontal tail surface
2 m
2
21.5 ft
2
Chord ratio
1
Horizontal tail span
2.45 m
8 ft
Elevator angle
25° ± 2°
Trim surface
0.08 m
2
0.86 ft
2
Vertical tail surface 1.12 m
2
12.05 ft
2
Rudder excursion
± 28° ± 2°
