Cessna 208B Grand Caravan G1000

536 Pages·2013·17.49 MB·English

CESSNA INTRODUCTION
MODEL 208B G1000
NOTICE
AT THE TIME OF ISSUANCE, THIS INFORMATION MANUAL
WAS AN EXACT DUPLICATE OF THE OFFICIAL PILOT’S
OPERATING HANDBOOK AND FAA APPROVED AIRPLANE
FLIGHT MANUAL AND IS TO BE USED FOR GENERAL
PURPOSES ONLY.
IT WILL NOT BE KEPT CURRENT AND, THEREFORE, CANNOT
BE USED AS A SUBSTITUTE FOR THE OFFICIAL PILOT’S
OPERATING HANDBOOK AND FAA APPROVED AIRPLANE
FLIGHT MANUAL INTENDED FOR OPERATION OF THE
AIRPLANE.
THE PILOT’S OPERATING HANDBOOK MUST BE CARRIED IN
THE AIRPLANE AND AVAILABLE TO THE PILOT AT ALL TIMES.
Revision 1 U.S. i
INTRODUCTION CESSNA
MODEL 208B G1000
PERFORMANCE - SPECIFICATIONS
CARGO VERSION
*SPEED (KTAS):
Maximum Cruise at 10,000 Feet . . . . . . . . . . . . . . . . . . . . 175 Knots
Maximum Cruise at 20,000 Feet . . . . . . . . . . . . . . . . . . . . 164 Knots
RANGE:With 2224 pounds usable fuel and fuel allowance for engine
start, taxi, takeoff, climb, descent and 45 minutes reserve.
Max Cruise at 10,000 Feet . . . . . . . . . . . . . . . . . . . . Range 862 NM
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 5.1 Hours
Max Cruise at 18,000 Feet . . . . . . . . . . . . . . . . . .Range - 1044 NM
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 6.6 Hours
Max Range at 10,000 Feet . . . . . . . . . . . . . . . . . . .Range - 963 NM
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 6.5 Hours
Max Range at 18,000 Feet . . . . . . . . . . . . . . . . . .Range - 1076 NM
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 7.0 Hours
RATE-OF-CLIMB AT SEA LEVEL . . . . . . . . . . . . . . . . . . . . . .925 FPM
SERVICE CEILING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22,800 Feet
MAXIMUM OPERATING ALTITUDE . . . . . . . . . . . . . . . . . 25,000 Feet
TAKEOFF PERFORMANCE:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1405 Feet
Total Distance Over 50 Foot Obstacle. . . . . . . . . . . . . . . . 2500 Feet
LANDING PERFORMANCE:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 915 Feet
Total Distance Over 50 Foot Obstacle. . . . . . . . . . . . . . . . 1740 Feet
STALL SPEED (KCAS):
Flaps Up, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78 Knots
Flaps Full, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 Knots
MAXIMUM WEIGHT:
Ramp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8785 Pounds
Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8750 Pounds
Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8500 Pounds
STANDARD EMPTY WEIGHT. . . . . . . . . . . . . . . . . . . . . 4680 Pounds
Maximum USEFUL LOAD . . . . . . . . . . . . . . . . . . . . . . . . 4105 Pounds
*Speeds are based on mid-cruise weight.
(Continued Next Page)
ii U.S. Revision 1
CESSNA INTRODUCTION
MODEL 208B G1000
PERFORMANCE - SPECIFICATIONS
CARGO VERSION (Continued)
WING LOADING . . . . . . . . . . . . . . . . . . . . . .31.3 Pounds/Square Foot
POWER LOADING . . . . . . . . . . . . . . . 13.0 Pounds/Shaft Horsepower
FUEL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 335.6 Gallons
OIL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 Quarts
ENGINE: Pratt & Whitney Canada . . . . . . . . . . . . . . . . . . . PT6A-114A
Free Turbine Flat Rated at 675 Shaft Horsepower
PROPELLER:
McCauley 3-bladed, Constant Speed,
Full Feathering, Reversible Propeller
Diameter. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 106 Inches
NOTE
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.
Revision 1 U.S. iii
INTRODUCTION CESSNA
MODEL 208B G1000
PERFORMANCE - SPECIFICATIONS
PASSENGER VERSION
* SPEED (KTAS):
Maximum Cruise at 10,000 Feet . . . . . . . . . . . . . . . . . . . . 184 Knots
Maximum Cruise at 20,000 Feet . . . . . . . . . . . . . . . . . . . . 174 Knots
RANGE:With 2224 pounds usable fuel and fuel allowance for engine
start, taxi, takeoff, climb, descent and 45 minutes reserve.
Max Cruise at 10,000 Feet . . . . . . . . . . . . . . . . . . .Range - 907 NM
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 5.1 Hours
Max Cruise at 18,000 Feet . . . . . . . . . . . . . . . . . . Range - 1109 NM
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 6.6 Hours
Max Range at 10,000 Feet . . . . . . . . . . . . . . . . . .Range - 1026 NM
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 6.6 Hours
Max Range at 18,000 Feet . . . . . . . . . . . . . . . . . . Range - 1163 NM
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 7.4 Hours
RATE-OF-CLIMB AT SEA LEVEL . . . . . . . . . . . . . . . . . . . . . .975 FPM
SERVICE SEALING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23,700 Feet
MAXIMUM OPERATING ALTITUDE . . . . . . . . . . . . . . . . . 25,000 Feet
TAKEOFF PERFORMANCE:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1365 Feet
Total Distance Over 50 Foot Obstacle . . . . . . . . . . . . . . . 2420 Feet
LANDING PERFORMANCE:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 950 Feet
Total Distance Over 50 Foot Obstacle. . . . . . . . . . . . . . . . 1795 Feet
STALL SPEED (KCAS):
Flaps Up, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78 Knots
Flaps Full, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 Knots
MAXIMUM WEIGHT:
Ramp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8785 Pounds
Takeoff. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8750 Pounds
Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8500 Pounds
STANDARD EMPTY WEIGHT. . . . . . . . . . . . . . . . . . . . . .4511 Pounds
Maximum USEFUL LOAD . . . . . . . . . . . . . . . . . . . . . . . . 4274 Pounds
*Speeds are based on mid-cruise weight.
(Continued Next Page)
iv U.S. Revision 1
CESSNA INTRODUCTION
MODEL 208B G1000
PERFORMANCE - SPECIFICATIONS
PASSENGER VERSION (Continued)
WING LOADING . . . . . . . . . . . . . . . . . . . . . .31.3 Pounds/Square Foot
POWER LOADING . . . . . . . . . . . . . . . 13.0 Pounds/Shaft Horsepower
FUEL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 335.6 Gallons
OIL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 Quarts
ENGINE: Pratt & Whitney Canada . . . . . . . . . . . . . . . . . . . PT6A-114A
Free Turbine Flat Rated at 675 Shaft Horsepower
PROPELLER:
McCauley 3-bladed, Constant Speed,
Full Feathering, Reversible. Diameter. . . . . . . . . . . . . . . . . 106 Inches
NOTE
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.
Revision 1 U.S. v/vi

CESSNA INTRODUCTION
MODEL 208B G1000
Cessna Aircraft Company
Model 208B G1000
This manual incorporates information issued in the Pilot's Operating
Handbook and FAA approved Airplane Flight Manual at Revision 1,
Dated 5 June 2008 (Part Number 208BPHBUS-01).
COPYRIGHT © 2008
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
208BIMBUS-01 U.S. vii/viii

CESSNA INTRODUCTION
MODEL 208B G1000
TABLE OF CONTENTS
SECTION
GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1
LIMITATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2
EMERGENCY PROCEDURES . . . . . . . . . . . . . . . . . .3
NORMAL PROCEDURES . . . . . . . . . . . . . . . . . . . . . .4
PERFORMANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5
WEIGHT AND BALANCE/EQUIPMENT LIST . . . . . . .6
AIRPLANE AND SYSTEM DESCRIPTION . . . . . . . . .7
HANDLING, SERVICE AND MAINTENANCE . . . . . . .8
SUPPLEMENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9
Revision 1 U.S. ix
INTRODUCTION CESSNA
MODEL 208B G1000
WARNINGS, CAUTIONS, AND NOTES
Throughout the text, warnings, cautions, and notes pertaining to
airplane handling and operations are utilized. These adjuncts to the text
are used to highlight or emphasize important points.
WARNING
Operating procedures, techniques, etc., which can
result in personal injury or loss of life if not
carefully followed.
CAUTION
Operating procedures, techniques, etc., which can
result in damage to equipment if not carefully followed.
NOTE
An operating procedure, technique, etc., which is
considered essential to emphasize.
x U.S. Revision 1