Airplane Flight Manual
Van’s Aircraft RV-7A
HB-YMT
7 Aeroplane and system description – Page 17
Edition 01.11.2017
7.12 Piot and static pressure systems
The single unheated Pitot tube below the left wing measures dynamic
pressure and feeds it to the following instruments:
•
Backup Airspeed Indicator
•
Air Data Computer part of the EFIS
•
Angle of Attack CPU
•
Trutrak Flight Systems Digiflight II VSGV Autopilot
The single static system measures outside static pressure on the left and
right side of the rear fuselage. It feeds into the following instruments:
•
Backup Airspeed Indicator
•
Backup Altimeter
•
Air Data Computer part of the EFIS
•
Angle of Attack CPU
•
Trutrak Flight Systems Digiflight II VSGV Autopilot
