Tecnam P2002 JF - Page 1063

2
nd
Edition - Rev 0
SUPPLEMENT SG-3
CHAPTER 31 - INDICATIONG SYSTEM
Page 11
Pitot/static system
The below figure shows a schematic of the Pitot/static system with the connec-
tions to the instruments and Air Data Computer.
Static line is connected with the GDC 74A, standby altimeter and standby air-
speed indicator.
The Pitot line is connected to GDC 74A unit and to the standby airspeed indicator.