Performance - Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook

CESSNA
MODELT210M
SECTION 5
PERFORMANCE
SECTION 5
PERFORMANCE
TABLE OF CONTENTS
Introduction . . . . . . .
Use Of Performance Charts
Sample Problem
Takeoff
Cruise . . . .
Fuel Required
Landing . . .
Figure 5-1, Airspeed Calibration - Normal Static Source
Airspeed Calibration - Alternate Static Source
Figure 5-2, Temperature Conversion Chart
Figure 5-3, Stall Speeds . . . . . . . . . . . . .
Figure 5-4, Takeoff Distance - 3800 Lbs . . . . . .
Takeoff Distance - 3500 Lbs And 3200 Lbs
Figure 5-5, Rate Of Climb - Maximum . . . . .
Figure 5-6, Time, Fuel, And Distance To Climb -
Maximum Rate Of Climb . . . .
Time, Fuel, And Distance To Climb -
Normal Climb . . . . . .
Figure 5-7, Cruise Performance - 2000 Feet
Cruise Performance - 4000 Feet
Cruise Performance - 6000 Feet
Cruise Performance - 8000 Feet
Cruise Performance - 10,000 Feet
Cruise Performance - 12,000 Feet
Cruise Performance - 14,000 Feet
Cruise Performance - 16,000 Feet
Cruise Performance - 18,000 Feet
Cruise Performance - 20,000 Feet
Cruise Performance - 22,000 Feet
Cruise Performance - 24,000 Feet
Figure 5-8, Range Profile . .
Figure 5-9, Endurance Profile
Figure 5-10, Landing Distance
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