Cessna 206H - SECTION 5 PERFORMANCE

SOLOY TURBINE PAC SECTION 5
POHS CESSNA T206H/206H PERFORMANCE
5-1
F.A.A. Approved May 23, 2003
SECTION 5
PERFORMANCE
TABLE OF CONTENTS .................................................... PAGE
Introduction ................................................................................. 5-3
Figure 5-1: Airspeed Calibration ................................................ 5-4
Figure 5-2: Temperature Conversion Chart ............................... 5-5
Figure 5-3: Stall Speeds ............................................................ 5-6
Figure 5-4: Minimum Engine Torque For Takeoff ...................... 5-8
Figure 5-5: Takeoff Distance, 3600 Lbs. ................................... 5-9
Figure 5-6: Takeoff Distance, 3300 Lbs. ............................. .... 5-11
Figure 5-7: Takeoff Distance, 3000 Lbs. .................................. 5-13
Figure 5-8: Maximum Rate of Climb, Maximum Continuous
Power .................................................................. 5-15
Figure 5-9: Maximum Rate of Climb, Takeoff Power .............. 5-16
Figure 5-10: Time, Fuel and Distance to Climb, Maximum
Rate of Climb, Maximum Continuous Power,
Temperature – Standard ................................... 5-17
Time, Fuel and Distance to Climb, Maximum
Rate of Climb, Maximum Continuous Power,
Temperature – Standard +20C ........................... 5-18
Time, Fuel and Distance to Climb, Maximum
Rate of Climb, Maximum Continuous Power,
Temperature – Standard -20C ........................... 5-19
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