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:
29/60
OIL PRESSURE
(min - max)
0.8 bar - 7 bar
(12 psi - 102 psi)
0.8 bar - 7 bar
(12 psi - 102 psi)
0.8 bar - 7 bar (12
psi - 102 psi)
OIL
PRESSURE
(normal
operating
range)
2.0 bar - 5.0 bar
(29 psi - 73 psi)
2.0 bar - 5.0 bar
(29 psi - 73 psi)
2.0 bar - 5.0 bar
(29 psi - 73 psi)
FUEL PRESSURE
(min - max)
0.15 bar - 0.4 bar
(2.2 psi - 5.8 psi)
0.15 bar - 0.4 bar
(2.2 psi - 5.8 psi)
2.8 bar - 3.2 bar
(40.5 psi - 46.5 psi)
COOLING LIQUID
120 °C / 248 °F
120 °C / 248 °F
120 °C / 248 °F
CHT
150 °C / 302 °F
135 °C / 275 °F
-
For detailed information on engine limitations, refer to the ROTAX operator's manual.
3.9. WEIGHT AND BALANCE LIMITATIONS
The values below are related to the aircraft structural and design limits which may not coincide with
the limit values of the national regulations on recreational flight. Therefore, it is strictly forbidden to
go beyond these limits to avoid problems, accidents and, moreover, legal problems.
Maximum take-off weight
M.T.O.W.
600 Kg / 1320 lbs
Maximum landing weight
M.L.W
600 Kg / 1320 lbs
Maximum baggage weight
90+90+20 Kg / 154+44 lbs
WARNING
CHECK THE MAXIMUM TAKE-OFF WEIGHT
LIMITS APPLICABLE ACCORDING TO THE
REGULATIONS OF THE STATE IN WHICH YOU
INTEND TO FLY.
The position of the center of gravity must remain within the following limits:
C.G. forward limit:
19% MAC
C.G. rear limit:
35% MAC
Note: MAC = Mean Aerodynamic Chord
The distance of the center of gravity from the leading edge of the wing is shown as a percentage of
the mean aerodynamic chord.
3.10. CREW
Minimum crew:
1 pilot
Maximum number of people on board:
2
