Textron Cessna Grand Caravan Ex 208B - Page 290

SECTION 5 CESSNA
PERFORMANCE MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
TABLE OF CONTENTS (Continued)
Page
AIRPLANES WITH CARGO POD INSTALLED
(Continued)
Fuel and Time Required - Maximum Cruise Power (40-200 NM) . 5-59
Fuel and Time Required - Maximum Cruise Power (200-1000 NM) 5-60
Fuel and Time Required - Maximum Range Power (40-200 NM) . 5-61
Fuel and Time Required - Maximum Range Power (200-1000 NM)5-62
Range Profile . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-63
Endurance Profile. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-64
Time, Fuel, and Distance to Descend . . . . . . . . . . . . . . . . . . . . . . 5-65
Short Field Landing Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-67
AIRPLANES WITHOUT CARGO POD
Short Field Takeoff Distance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-72
Flaps UP Takeoff Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-77
Rate of Climb - Takeoff Flap Setting. . . . . . . . . . . . . . . . . . . . . . . . 5-80
Climb Gradient - Takeoff Flap Setting . . . . . . . . . . . . . . . . . . . . . . 5-81
Maximum Rate of Climb - Flaps UP. . . . . . . . . . . . . . . . . . . . . . . . 5-82
Climb Gradient - Takeoff - Flaps UP. . . . . . . . . . . . . . . . . . . . . . . . 5-83
Cruise Climb - Flaps UP - 115 KIAS. . . . . . . . . . . . . . . . . . . . . . . . 5-84
Rate of Climb - Balked Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-85
Time, Fuel, and Distance to Climb - Maximum Rate of Climb . . . . 5-87
Time, Fuel, And Distance to Climb - Cruise Climb - 115 KIAS . . . . 5-88
Cruise Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-89
Cruise Maximum Torque . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-101
Fuel and Time Required Maximum Cruise Power (40-200 NM). . 5-108
Fuel and Time Required Maximum Cruise Power (200-1000 NM) 5-109
Fuel and Time Required Maximum Range Power (40-200 NM) . .5-110
Fuel and Time Required Maximum Range Power (200-1000 NM) 5-111
Range Profile . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5-112
Endurance Profile. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5-113
Time, Fuel, and Distance to Descend . . . . . . . . . . . . . . . . . . . . . .5-114
Short Field Landing Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5-115
208BPHCUS-00
5-2