CESSNA SECTION 5
MODEL 208B 867 SHP PERFORMANCE
GARMIN G1000
U.S.
FAA APPROVED
MAXIMUM ENGINE TORQUE FOR TAKEOFF
1. Torque increases approximately 30 FT-LB from 0 to 60 KIAS.
2. Torque on this chart shall be achieved without exceeding
850°C ITT or 103.7 percent N
g
. When the ITT exceeds 825°C,
this power setting is time limited to 5 minutes.
3. With the inertial separator in BYPASS, where altitude and
temperature do not permit 2397 FT-LB for takeoff, decrease
torque setting by 85 FT-LB.
4. With the cabin heater ON, where altitude and temperature do
not permit 2397 FT-LB for takeoff, decrease torque setting by
75 FT-LB.
Figure 5-8 (Sheet 2
208BPHCUS-00
5-21
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