AEROPRAKT 22LS, Руководство по эксплуатации для пилотов

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AEROPRAKT-22LS Pilot Operating Handbook A22LS-POH-04
8.9 Full and static pressure system
This system supplies the full (dynamic) and static pressure of the outside air to the
instruments measuring the flight parameters: airspeed, rate of climb and altitude. The
system consists of the full and static pressure probe 1 and full 2 and static 3 pressure lines
connecting the probe to the instruments (see Fig. 11 ). Full and static pressure lines have
joints 4 used to disconnect the lines when the left wing is removed during aircraft
disassembly.
The full and static pressure lines are connected to the airspeed indicator. The altimeter and
vertical speed indicator are connected to the static pressure line.
Good condition of the full and static pressure system is important for correct measurement
of the flight parameters and therefore for flight safety. Pilots must take measures to keep
the system in good condition: protect the full and static pressure probe with a cover
(marked with a red "Remove before flight" flag) and inspect the probe and lines during the
preflight check to make sure that they are not damaged or blocked (by water, ice, dirt, etc.).
Fig. 11. Full and static pressure system
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