DIAMOND AIRCRAFT
HK 3 6 TS
FLIGHT MANUAL
7 . 12 PITOT
AND
STATIC SYSTEM
Systems Description
Static pres sure , total head and the pressure for the compensation
of the vertical speed indicator are measured by means of a Pi tot tube
which i s mounted to the vertical s tabil i zer . The tube i s removable .
A safe connection of the l ines i s established automat ically when the
Pi tot tube is inserted to the stop in the mount .
The lowest spot of the Pitot and s tatic l ines i s bridged by means
of bypas s l ines . Water that might have entered the system can
accumulate there . Removal of water must be done during scheduled
inspections ( refer to Maintenance Manual ) .
For the operation of additional avionic s , refer to the manual s of
the respective manufacturers .
7 . 14
PLACARDS
INSCRIPTIONS
The l imitation placards are presented in paragraph 2 . 15 . A l i s t of
all placards and inscriptions i s included in the Maintenance Manual .
Revis ion No .
Date
Source
Doc . No .
I s sue
Page No .
3 . 0 1 . 0 6
Jan 1 9 9 6
7 - 1 6
