CESSNA
MODEL 208B 867 SHP
GARMIN G1000
MAXIMUM ENGINE TORQUE FOR CLIMB
1. Torque on this chart shall be achieved without exceeding
825°C ITT or 103.7 percent N
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.
FAA APPROVED
208BPHCUS-00
NOTE
.
g
Figure 5-9 Sheet 2
SECTION 5
PERFORMANCE
U.S.
5-23