Flugzeugbau Ventus-2C - 7.6 Static Pressure and Pitot Pressure System

SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2c FLIGHT MANUAL
7.6 Static pressure and Pitot pressure system
Static pressure sources
a) Static pressure ports are on either side of the fuselage tail boom,
0.8 m (31.5 in.) forward of the base of the fin (in the horizontal plane) and
0.15 m (5.9 in.) below the fuselage-to-wing fillet (to be used for airspeed
indicator etc.).
b) On request a special static pressure probe can be installed near the top of
the fin (for further instruments, except ASI).
Pitot pressure sources
The Pitot pressure head is near the top of the fin
(to be used for airspeed indicator and other instruments).
November 2003
Revision -- 7.6
ASI
ALTIMETER
STATIC pressure
PITOT pressure
STATIC pressure
(Option)