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:
28/60
3.6. DESIGN LOAD FACTORS
Limit load factor at 600 Kg (1320 lbs):
Retracted flaps +4.0 g / -2.0 g
Extended flaps +2.0 g / 0 g
Safety factor for the ultimate load: 1.5.
WARNING
LOAD THE VENTURA MORE THAN 600 KG IT IS
FORBIDDEN. THE STRUCTURE HAS NOT BEEN
DESIGNED AND TESTED FOR HIGHER LOADS.
THE DESIGN LIMIT EXCEEDS THE NATIONAL
(ITALIAN) REGULATIONS FOR RECREATIONAL
FLIGHT; OBSERVE THE MOST STRINGENT
REGULATION.
3.7. PROHIBITED MANEUVERS
Acrobatic maneuvers included spins are not allowed. The aircraft must be operated according to the
Visual Flight Rules (VMC conditions) in direct ground contact. Night or Instrumental Flight (with IMC)
are not allowed.
WARNING
AEROBATIC IS FORBIDDEN.
FLYING
WITH
INSTRUMENTAL
FLIGHT
CONDITIONS AND WITHOUT GROUND VISUAL
CONTACT IT’S FORBIDDEN.
3.8. ENGINE LIMITATIONS (data source: Rotax manuals)
912UL
912ULS
912iS / 914UL / 915iS
RPM MAX
5800 RPM (5’max)
5800 RPM (5’max)
5800 RPM (5’max)
RPM
MAX
CONTINUOUS
5500 RPM
5500 RPM
5500 RPM
OIL
TEMPERATURE
(min - max)
50 °C - 140 °C
(122 °F - 285 °F)
50 °C - 130 °C
(122 °F - 266 °F)
50 °C - 130 °C
(122 °F - 266 °F)
OIL
TEMPERATURE
(normal
operating
range)
90 °C - 110 °C
(190 °F - 230 °F)
90 °C - 110 °C
(190 °F - 230 °F)
90 °C - 110 °C
(190°F - 230 °F)
