Tecnam P2010 - Pitot-Static Pressure Systems

Page 7 - 24
2
nd
Edition, Rev 0
Section 7 – Airframe and Systems description
PITOT-STATIC PRESSURE SYSTEMS
10. PITOT-STATIC PRESSURE SYSTEMS
The P2010 air speed/altitude indicating systems are connected with a Pitot-Static sys-
tem based on a total pressure/Pitot probe (simple Pitot 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 G1000 suite and standby MD 302 unit are connected to both static and total
pressure lines providing both air speed and altitude information.
GARMIN G1000
LH STATIC PORT
RH STATIC PORT
"T" JOINT
MD-302
ALTERNATE STA TIC PORT
ALTERNATE STA TIC PORT VALVE
GDC 74A
ADC
1
2
3
4
Pos.
Description
1
2
3
4
Pitot
"T" Joint
Garmin G1000 connection
MD-302
0°
T/O
LND
FLAP
FIG.7-16. PITOT-STATIC SYSTEM
Legenda:
Static line
Total line