Aircraft Systems
LIGHTS
AL250 Flight Manual
MEP
6-11-1 ALTERNATE STATIC VALVE
In the event of a failure of the Pitot static system (due to blocking, possibly with ice),
the static pressure in the cabin can alternatively be used as the static pressure source.
The Alternate Static Valve control is located below the instrument panel to the lower
left of the left-side pilot’s control wheel. Rotating the valve to point towards the pilot
allows the static source to b e taken from inside the cabin.
Figure 6.62: Alternate Static Valve Control
6-12 LIGHTS
Figure 6.63: Light switches on the dashboard
The following light switches are located on the left-hand side of the dashboard:
• Landing lights
• Taxi lights
• Navigation lights
• Strobe lights
The position of the light switches influences not only the simulated aircraft electrical
requirements but also the visual syste m outside, except for the navigation lights.
Rev. 1.8 © 2021 ALSIM - All Rights Reserved 6-65
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