10.
PITOT-STATIC
PRESSURE
SYSTEMS
The P20 I 0 air speed/altitude indicating systems are connected with a Pilot-Static sys-
tem based on a total pressure/Pilot probe (simple Pilot tube, heated for icing protec-
tion) mounted on left wing strut and two static pressure ports connected
in
parallel
and located
in
correspondence
of
engine firewall on left and right side
of
fuselage.
Flexible hoses connects total pressure and static ports
to
primary analogue instru-
ments, anemometer and altimeter.
Garmin
GIOOO
suite and standby MD 302 unit are connected
to
both static and total
pressure lines providing both air speed and altitude information.
r -
r
-,
l.. ..JQ)
Legenda
:
Static
line
- Totalline
Description
Gannin
GlOOO
connecuon
4
MD
-
302
FIG.7-16.
PITOT-STATIC
SYSTEM
2"d
Edlllon, Rev 0
Section
7 -
Airframe
and
Systems
description
PITOT-STATIC
PRESSURE
SYSTEMS
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