SOLOY TURBINE PAC
POHS CESSNA T206H/206H
feet, the desired vacuum is 4.5 to 5.5 inches of mercury. A
vacuum reading out of this range at altitudes below 15,000 feet
may indicate a system malfunction or improper adjustment, and in
this case, the indicators should not be considered reliable. At
15,000 feet and above, the vacuum gage may indicate below 4.5
in. Hg. and still be adequate for normal vacuum system operation.
A minimum vacuum gauge reading of 4.5 in. Hg is acceptable at
15,000 feet; for each additional 5000 foot altitude increment, up to
30,000 feet, a decrease of 0.5 in. Hg. is acceptable.
LOW VACUUM ANNUNCIATION – No Change
CLOCK/O.A.T. INDICATOR
STALL WARNING SYSTEM –
STANDARD AVIONICS –
AVIONICS SUPPORT EQUIPMENT –
CABIN FEATURES –
F.A.A. Approved
AIRPLANE & SYSTEMS
– No Change
No Change
No Change
No Change
7-26
SECTION 7
DESCRIPTION
No Change
May 23, 2003