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BELL HELICOPTER BELL 430 - condensation drains; dual static ports; pitot tube

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41
THIS IS AN UNCONTROLLED DOCUMENT.
THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.
THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE
FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.
PRODUCT DATA JANUARY 2003
The alternate static source switch is located on the lower right side of the center pedestal.
Since a second external source is provided there in no need for an
internal source,
which could cause
inaccurate instrument indications.
Additionally, a second pitot tube is installed
as
standard equipment. Located on the left
side of the nose, but not connected
internally, it is included to facilitate
installation of the optional copilot
instrument kit. The pitot-static system is
fitted with condensation drains and
provisions to attach standard flight
instrument ground calibration test
equipment.
DUAL STATIC PORTS
PITOT TUBE
PRI / ALT STATIC SOURCE
SELECT SWITCH

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