SECTION 5 CESSNA
PERFORMANCE MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
SAMPLE PROBLEM (Continued)
TAKEOFF (Continued)
The Maximum Engine Torque For Takeoff chart should be consulted for
takeoff power setting. For the above ambient conditions, the power
setting is:
The Maximum Engine Torque For Climb chart should be consulted for
climb power setting from field elevation to cruise altitude. For the above
ambient conditions, the power setting is:
Takeoff Torque 2397 FT-LB
Field Elevation Maximum Climb Torque
2189 FT-LB
Cruise Altitude Maximum Climb Torque 1713 FT-LB
208BPHCUS-00
5-6
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