CHAPTER 34
PAGE 4
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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
PAGE DATE: 1. July 1996
34-10-00 FLIGHT ENVIRONMENT DATA
This Section describes that portion of the system which
senses the environmental conditions and uses the data to
influence navigation.
34-10-01 Pitot/Static System
The pitot/static tube is designed to pick up pitot pressure
and static pressure. It is screwed through the L.H. outboard
leading edge into an attachment block located at the rear
web of the main spar. From there the pressures are transmit-
ted by means of a vinyl tubing which is routed through an
aluminium tube inside the wing to the left side of the
fuselage and further to the instrument panels. The ends of
each vinyl tube are marked with the letters "P" or "S" for
pitot resp. static pressure line. The pitot/static system can
be drained by means of an U-shaped drain which is located
at the left side of the cockpit as shown in Figure 1.
Pitot/Static Drain
Figure 1
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