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1.10 Pitot and Static Pressure Systems
The airspeed indicator system for the aircraft is shown below.
On the left wing’s strut the Pitot tube (1) while on the fuselage’s sides there are two static ports (2). Two flexible hoses (3)
feed the airspeed indicator (4), the altimeter (5) and the VSI (6) on the instrument panel.
Fig.1-5 Pitot Static system
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