SOLOY TURBINE PAC SECTION 7
POHS CESSNA T206H/206H AIRPLANE & SYSTEMS
DESCRIPTION
7-26
F.A.A. Approved May 23, 2003
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 – No Change
STALL WARNING SYSTEM – No Change
STANDARD AVIONICS – No Change
AVIONICS SUPPORT EQUIPMENT – No Change
CABIN FEATURES – No Change
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