NOTICE

SECTION 5 CESSNA
PERFORMANCE MODEL 208B G1000
TABLE OF CONTENTS (Continued) Page
Cruise Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-35
Cruise Maximum Torque . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-46
Fuel and Time Required - Maximum Cruise Power (40-200 NM) . 5-53
Fuel and Time Required - Maximum Cruise Power (200-1000 NM) 5-54
Fuel and Time Required - Maximum Range Power (40-200 NM) . 5-55
Fuel and Time Required - Maximum Range Power (200-1000 NM) 5-56
Range Profile . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-57
Endurance Profile. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-58
Time, Fuel, and Distance to Descend . . . . . . . . . . . . . . . . . . . . . . 5-59
Short Field Landing Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-60
Airplanes Without Cargo Pod
Short Field Takeoff Distance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-65
Flaps UP Takeoff Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-70
Rate of Climb - Takeoff Flap Setting. . . . . . . . . . . . . . . . . . . . . . . . 5-73
Climb Gradient - Takeoff Flap Setting . . . . . . . . . . . . . . . . . . . . . . 5-74
Maximum Rate of Climb - Flaps UP . . . . . . . . . . . . . . . . . . . . . . . . 5-75
Climb Gradient - Takeoff - Flaps UP. . . . . . . . . . . . . . . . . . . . . . . . 5-76
Cruise Climb - Flaps UP - 115 KIAS. . . . . . . . . . . . . . . . . . . . . . . . 5-77
Rate of Climb - Balked Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-78
Time, Fuel, and Distance to Climb - Maximum Rate of Climb . . . . 5-79
Time, Fuel, And Distance to Climb - Cruise Climb - 115 KIAS . . . . 5-80
Cruise Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-81
Cruise Maximum Torque . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-93
Fuel and Time Required Maximum Cruise Power (40-200 NM). . 5-100
Fuel and Time Required Maximum Cruise Power (200-1000 NM) 5-101
Fuel and Time Required Maximum Range Power (40-200 NM) . 5-102
Fuel and Time Required Maximum Range Power (200-1000 NM) 5-103
Range Profile . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-104
Endurance Profile. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-105
Time, Fuel, and Distance to Descend . . . . . . . . . . . . . . . . . . . . . 5-106
Short Field Landing Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-107
5-2
U.S.
FAA APPROVED
208BPHBUS-00