SECTION 4 CESSNA
NORMAL PROCEDURES MODEL T182T NAV III
GFC 700 AFCS
U.S.
CRUISE (Continued)
LEANING USING TURBINE INLET TEMPERATURE (T.I.T.)
(Continued)
When cruising at altitudes above 15,000 feet, the maximum
allowable manifold pressure is 27 in.hg. due to detonation
restrictions. Refer to Section 5, cruise tables for operational
power settings.
Certain considerations must be made when using a T.I.T. indicator.
Operations that are not approved include:
1. Cruise power settings above the green arc range limitation.
2. Operations at T.I.T. indications above 1685°F.
3. Mixture settings that cause engine roughness or excessive
power loss to occur.
(Continued Next Page)
T182TPHBUS-00
4-38
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