Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 7

CESSNA
MODEL 208B (867 SHP)
GARMIN G1000
PERFORMANCE - SPECIFICATIONS
CARGO VERSION
MAXIMUM WEIGHT:
Ramp. . . . . . . . . . . . . . . . . . . . . . . . . . . 8842 POUNDS (4010.7 kg)
Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . 8807 POUNDS (3994.8 kg)
Landing . . . . . . . . . . . . . . . . . . . . . . . . . 8500 POUNDS (3855.5 kg)
STANDARD EMPTY WEIGHT. . . . . . . . . . 4558 POUNDS (2067.5 kg)
MAXIMUM USEFUL LOAD . . . . . . . . . . . . 4284 POUNDS (1943.2 kg)
WING LOADING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31.5 lbs/sq. ft.
POWER LOADING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.2 lbs/SHP
FUEL CAPACITY . . . . . . . . . . . . . . . . . . . . . 335.6 GALLONS (1270.0 l)
OIL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 QUARTS (13.2 l)
ENGINE: Pratt & Whitney Canada . . . . . . . . . . . . . . . . . . . . PT6A-140
Free Turbine Flat Rated at 867 SHP
PROPELLER: Hartzell Propeller Systems
3-bladed, Constant Speed, Full Feathering, Reversible Propeller
Diameter. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 106 Inches (2.7 m)
The above performance figures are based on indicated weights,
standard atmospheric conditions, level, hard-surfaced dry runways and
no wind. They are calculated values derived from flight tests conducted
by Cessna Aircraft Company under carefully documented conditions
and will vary with individual airplanes and numerous factors affecting
flight performance.
Performance for other operational conditions can be derived by
reference to operational data in other sections of this POH/AFM.
208BPHCUS-00
(Continued)
INTRODUCTION
U.S. v