文档介绍：Aircraft Operation Manual
Cessna 208A
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Aircraft Operation Manual Cessna 208A
Number of Airplanes : 1
Registration : D-FOLE Version : 675A Built: 1995 Configuration : Combi
History
Version : Caravan 675 A
Date of first flight : August 11, 1995
First Aircraft for Airlines : November 13,1999
Technical Specifications
Performance
Certified Ceiling 25,000 feet / 7,620 m
Cruise Speed (10,000 ft) 186 kts / 344 km
Range (10,000 ft)
932 NM / 1,726 km
Includes takeoff, climb, cruise, descent and
45- at power
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Aircraft Operation Manual Cessna 208A
Rate of Climb 1234 feet / 376 m
Stall Speed (Ldg) 61 kts / 113 km
Takeoff Roll ISA 1160 feet / 354 m
Landing Roll 1655 feet / 504 m
Weights
Maximum Useful Load 4,062 lbs /1,842 kg
Maximum Weights
8,035 lbs / 3,645 kg
Ramp
8,000 lbs / 3,629 kg
Takeoff
7,000 lbs / 3,538 kg
Landing
Power Loading 11,9 lbs / Hp
Standard Empty Weight 3,973 lbs /1,802 kg
Wing Loading 28,6 Lbs / sq ft
Dimensions
Cabin (Aft of Pilot Area)
Length 12,7 feet / 3,7 m
Height 4,3 Feet / 1,30 m
Width 5,2 feet / 1,6 m
Volume cu 254 feet / cu m
Optional Cargo Pod (External)
Weight Limits 1,090 lbs / kg
Volume cu feet / cu m
Overall Dimensions
Length 37,6 feet / 11,50 m
Span feet / 15,1 m
Height feet / m
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Aircraft Operation Manual Cessna 208A
Engine
Manufacturer Pratt & Whitney
Model PT6A-114A
Fuel Capacity 335 gal / 2,248 lbs
3-Bladed, ConstantSpeed, Full Feathering,
Propeller
Reversible
SHP 675
The small PT6 is a lightweight turboprop reverse-flow engine providing a power range from
580 to 920 shaft horsepower (ESHP).
It is the most popular gas turbine engine in its class. Since production started in 1964, more
than 60 versions of the PT6 engine have been certified.
The engine is installed in many different aircraft models used fo