AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGRATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 7-24
10. PITOT-STATIC PRESSURE SYSTEMS
The P2010 air speed/altitude indicating systems are connected with a Pitot-Static
system based on a total pressure/Pitot probe (simple Pitot tube, heated for icing
protection) 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 ana-
logue instruments, anemometer and altimeter.
Garmin G500 suite and standby MD 302 unit are connected to both static and to-
tal pressure lines providing both air speed and altitude information.
0°
T /O
LND
F LAP
LH STATIC PORT
RH STATIC PORT
"T" JOINT
ALTERNATE STATIC PORT
ALTERNATE STATIC PORT VALVE
GARMIN G500
GDC 74A
ADC
MD-302
G500
0°
T/O
LND
FL AP
GDC 74A
ADC
G500
1
2
4
3
Pos. Description
1
2
3
4
Pitot
"T" Joint
Garmin G500 connection
MD-302
FIG.7-16. PITOT-STATIC SYSTEM
Legend:
Ed. 1Rev 0
Section 7 – Airframe and Systems description
PITOT-STATIC PRESSURE SYSTEMS
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