SECTION 7
“AERO” Sp. z o.o.
DESCRIPTION OF THE AEROPLANE
AT-3 R100
AND ITS EQUIPMENT
Page 7-26
JULY, 2010
AEROPLANE FLIGHT MANUAL
7.11. Pitot and static pressure systems
The sensors [9] and [8] receive air under pitot and static pressure and
transmit it to the airspeed indicator [3], altimeter [2] , vertical speed
indicator [1] and altitude encoder[7](option) -see the scheme on the
illustration. The sensors of pitot and static pressure are fixed under
the port wing. Water sediment containers [6] are installed to both the
static pressure line [5] and to the pitot pressure line [4]. The sediment
containers are located beneath the pilot’s seat and are accessible
from outside.
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