CESSNA SECTION 5
MODEL 208B 867 SHP PERFORMANCE
GARMIN G1000
U.S.
FAA APPROVED
MAXIMUM ENGINE TORQUE FOR CLIMB
1. Torque on this chart shall be achieved without exceeding
825°C ITT or 103.7 percent N
g
.
2. With the inertial separator in BYPASS, decrease torque setting
by 115 FT-LB.
3. With the cabin heater ON, decrease torque setting by 85 FT-
LB.
Figure 5-9 Sheet 2
208BPHCUS-00
5-23
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