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  • CESSNA INTRODUCTIONMODEL 208 G1000

    U.S.

    NOTICE

    AT THE TIME OF ISSUANCE, THIS INFORMATION MANUALWAS AN EXACT DUPLICATE OF THE OFFICIAL PILOTSOPERATING HANDBOOK AND FAA APPROVED AIRPLANEFLIGHT MANUAL AND IS TO BE USED FOR GENERALPURPOSES ONLY.

    IT WILL NOT BE KEPT CURRENT AND, THEREFORE, CANNOTBE USED AS A SUBSTITUTE FOR THE OFFICIAL PILOTSOPERATING HANDBOOK AND FAA APPROVED AIRPLANEFLIGHT MANUAL INTENDED FOR OPERATION OF THEAIRPLANE.

    THE PILOTS OPERATING HANDBOOK MUST BE CARRIED INTHE AIRPLANE AND AVAILABLE TO THE PILOT AT ALL TIMES.

    Revision 1 i

  • INTRODUCTION CESSNAMODEL 208 G1000

    U.S.

    PERFORMANCE - SPECIFICATIONSWITHOUT CARGO POD

    *SPEED (KTAS):Maximum Cruise at 10,000 Feet . . . . . . . . . . . . . . . . . . . . 186 KnotsMaximum Cruise at 20,000 Feet . . . . . . . . . . . . . . . . . . . . 174 KnotsRANGE: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 932 NM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 5.1 HoursMax Cruise at 20,000 Feet . . . . . . . . . . . . . . . . . . Range - 1220 NM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 7.1 HoursMax Range at 10,000 Feet . . . . . . . . . . . . . . . . . . Range - 1085 NM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 7.0 HoursMax Range at 20,000 Feet . . . . . . . . . . . . . . . . . . Range - 1295 NM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 8.3 Hours

    RATE-OF-CLIMB AT SEA LEVEL . . . . . . . . . . . . . . . . . . . . .1234 FPMMAXIMUM OPERATING ALTITUDE . . . . . . . . . . . . . . . . . 25,000 FeetTAKEOFF PERFORMANCE:

    Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1160 FeetTotal Distance Over 50 Foot Obstacle . . . . . . . . . . . . . . . . 2055 Feet

    LANDING PERFORMANCE:Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 715 FeetTotal Distance Over 50 Foot Obstacle . . . . . . . . . . . . . . . . 1625 Feet

    STALL SPEED (KCAS):Flaps Up, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 KnotsFlaps Full, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 Knots

    MAXIMUM WEIGHT:Ramp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8035 PoundsTakeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8000 PoundsLanding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7800 Pounds

    STANDARD EMPTY WEIGHT . . . . . . . . . . . . . . . . . . . . . 4230 Pounds

    MAXIMUM USEFUL LOAD . . . . . . . . . . . . . . . . . . . . . . . 3805 Pounds

    * Speeds are based on mid-cruise weight.

    (Continued Next Page)

    Revision 1ii

  • CESSNA INTRODUCTIONMODEL 208 G1000

    U.S.

    PERFORMANCE - SPECIFICATIONSWITHOUT CARGO POD (Continued)

    WING LOADING . . . . . . . . . . . . . . . . . . . . . . 28.6 Pounds/Square FootPOWER LOADING . . . . . . . . . . . . . . . 11.9 Pounds/Shaft HorsepowerFUEL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 335.6 Gallons OIL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 QuartsENGINE:Pratt & Whitney Canada . . . . . . . . . . . . . . . . . . . . . . . . . . . PT6A-114A

    Free Turbine Flat Rated at 675 Shaft HorsepowerPROPELLER:McCauley 3-bladed, Constant Speed,

    Full Feathering, Reversible Propeller Diameter. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 106 Inches

    NOTEThe above performance figures are based on indicatedweights, standard atmospheric conditions, level, hard-surfaced dry runways and no wind. They are calculatedvalues derived from flight tests conducted by CessnaAircraft Company under carefully documented conditionsand will vary with individual airplanes and numerous factorsaffecting flight performance. Performance for otheroperational conditions can be derived by reference tooperational data in other sections of this POH/AFM.

    Revision 1 iii

  • INTRODUCTION CESSNAMODEL 208 G1000

    U.S.

    PERFORMANCE - SPECIFICATIONSWITH CARGO POD

    * SPEED (KTAS):Maximum Cruise at 10,000 Feet . . . . . . . . . . . . . . . . . . . . 177 KnotsMaximum Cruise at 20,000 Feet . . . . . . . . . . . . . . . . . . . . 165 KnotsRANGE: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 - 891 NM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 5.1 HoursMax Cruise at 20,000 Feet . . . . . . . . . . . . . . . . . . Range - 1155 NM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 7.1 HoursMax Range at 10,000 Feet . . . . . . . . . . . . . . . . . . Range - 1028 NM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 6.9 HoursMax Range at 20,000 Feet . . . . . . . . . . . . . . . . . . Range - 1199 NM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 7.9 Hours

    RATE-OF-CLIMB AT SEA LEVEL . . . . . . . . . . . . . . . . . . . . . 1175 FPMMAXIMUM OPERATING ALTITUDE . . . . . . . . . . . . . . . . . 25,000 FeetTAKEOFF PERFORMANCE:

    Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1170 FeetTotal Distance Over 50 Foot Obstacle . . . . . . . . . . . . . . . 2090 Feet

    LANDING PERFORMANCE:Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 710 FeetTotal Distance Over 50 Foot Obstacle . . . . . . . . . . . . . . . . 1600 Feet

    STALL SPEED (KCAS):Flaps Up, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 KnotsFlaps Full, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 Knots

    MAXIMUM WEIGHT:Ramp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8035 PoundsTakeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8000 PoundsLanding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7800 Pounds

    STANDARD EMPTY WEIGHT . . . . . . . . . . . . . . . . . . . . . 4230 PoundsMAXIMUM USEFUL LOAD . . . . . . . . . . . . . . . . . . . . . . . 3805 Pounds

    * Speeds are based on mid-cruise weight.

    (Continued Next Page)

    Revision 1iv

  • CESSNA INTRODUCTIONMODEL 208 G1000

    U.S.

    PERFORMANCE - SPECIFICATIONSWITH CARGO POD (Continued)

    WING LOADING . . . . . . . . . . . . . . . . . . . . . . 28.6 Pounds/Square FootPOWER LOADING . . . . . . . . . . . . . . . 11.9 Pounds/Shaft HorsepowerFUEL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 335.6 GallonsOIL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 QuartsENGINE: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

    NOTEThe above performance figures are based on indicatedweights, standard atmospheric conditions, level, hard-surfaced dry runways and no wind. They are calculatedvalues derived from flight tests conducted by CessnaAircraft Company under carefully documented conditionsand will vary with individual airplanes and numerous factorsaffecting flight performance. Performance for otheroperational conditions can be derived by reference tooperational data in other sections of this POH/AFM.

    Revision 1 v/vi

  • CESSNA INTRODUCTIONMODEL 208 G1000

    U.S.

    Cessna Aircraft Company

    Model 208 G1000

    This manual incorporates information issued in the Pilot's OperatingHandbook and FAA approved Airplane Flight Manual at Revision 1,Dated 5 June 2008 (Part Number 208PHBUS-01).

    COPYRIGHT 2008CESSNA AIRCRAFT COMPANY

    WICHITA, KANSAS, USA

    208IMBUS-01 vii/viii

  • CESSNA INTRODUCTIONMODEL 208 G1000

    U.S. xv

    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

    208PHBUS-02

  • INTRODUCTION CESSNA MODEL 208 G1000

    U.S.xvi

    This Page Intentionally Left Blank

    208PHBUS-02

  • CESSNA SECTION 1MODEL 208 G1000 GENERAL

    U.S. 1-1

    GENERAL

    TABLE OF CONTENTSPage

    Three View. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1-3Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1-5Descriptive Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1-6

    Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1-6Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1-6Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . .