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:
22/60
Ventilation / Heating
Two ventilation doors are placed in the side of front cabin compartment. Two rods located under the
side of instrument panel can control the ventilation flow.
Heating valve is moved by a panel-mounted lever that controls the inflow of hot air coming from the
engine compartment. Air enters in the cabin from a fireproof nozzle at the passenger's feet.
Pitot e static port
The system provides static pressure to the airspeed, altimeter, variometer, and dynamic pressure to
the airspeed. Static ports are placed on rear fuselage sides and the total port probe is on the left
wing leading edge next to the strut.
WARNING
WHEN THE AIRCRAFT IS ON THE GROUND,
PROTECT THE PITOT TUBE TO PREVENT ITS
OBSTRUCTION BY FOREIGN BODIES AND
REDUCE THE RISK OF DAMAGE OR INJURY DUE
TO ACCIDENTAL IMPACT.
Airspeed indicator markings
Airspeed indicator markings and their color-code significance are shown below:
Marking
Speed range
[mph]
Speed range
[km/h]
Speed range
[kt]
Notes
WHITE ARC
37-71
60-115
32-62
Extended flaps speed operation
GREEN ARC
44-112
70-180
38-97
Normal Operating Range
YELLOW ARC
112-143
180-230
97-124
Manoeuvres must be conducted
with caution and only in smooth
air.
RED LINE
143
230
124
Never exceed speed
Standard Basic instrumentation
The position of the basic instruments in standard configuration is shown below.
NOTE
The instrument panel arrangement may vary with
optional instruments.
