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Stall speeds for flaps-up and flaps-full conditions, maximum weights, wing and power loading, fuel and oil capacities are also specified, with notes clarifying the basis of the figures under standard conditions.",{"@graph":14,"@context":73},[15,34,56],{"@type":16,"itemListElement":17},"BreadcrumbList",[18,23,27,31],{"item":19,"name":20,"@type":21,"position":22},"https://docshare.wps.com","Home","ListItem",1,{"item":24,"name":25,"@type":21,"position":26},"https://docshare.wps.com/document/","Document",2,{"item":28,"name":29,"@type":21,"position":30},"https://docshare.wps.com/document/technology/","Technology",3,{"item":32,"name":10,"@type":21,"position":33},"https://docshare.wps.com/document/cessna-introduction-model-208b-g1000-performance-specifications-cargo-version/652756/",4,{"url":32,"name":10,"@type":35,"image":36,"author":41,"headline":10,"publisher":44,"fileFormat":47,"inLanguage":8,"description":12,"dateModified":48,"datePublished":49,"encodingFormat":47,"isAccessibleForFree":50,"interactionStatistic":51},"DigitalDocument",{"url":37,"@type":38,"width":39,"height":40},"https://docshare.wps.com/thumbnails/cessna-introduction-model-208b-g1000-performance-specifications-cargo-version/652756.png","ImageObject",300,407,{"name":42,"@type":43},"RuangKosong","Person",{"url":19,"name":45,"@type":46},"DocShare","Organization","application/pdf","2026-10-30","2026-10-24",true,{"@type":52,"interactionType":53,"userInteractionCount":55},"InteractionCounter",{"@type":54},"ViewAction",6,{"@type":57,"mainEntity":58},"FAQPage",[59,65,69],{"name":60,"@type":61,"acceptedAnswer":62},"What does the manual caution about using this information as a substitute?","Question",{"text":63,"@type":64},"It states that the information manual is an exact duplicate at issuance, is not kept current, and cannot be used as a substitute for the official Pilot’s Operating Handbook and FAA approved Airplane Flight Manual.","Answer",{"name":66,"@type":61,"acceptedAnswer":67},"What cruise speeds and ranges are given for the cargo version?",{"text":68,"@type":64},"The cargo version provides maximum cruise speeds at 10,000 and 20,000 feet, along with range values and time estimates for those cruise profiles.",{"name":70,"@type":61,"acceptedAnswer":71},"How are the performance numbers qualified in the manual?",{"text":72,"@type":64},"It notes the figures are based on indicated weights, standard atmospheric conditions, level hard-surfaced dry runways, and no wind, and they are calculated from flight tests under documented 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OF THE OFFICIAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL AND IS TO BE USED FOR GENERAL PURPOSES ONLY.  \nIT 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.  \nTHE PILOT’S OPERATING HANDBOOK MUST BE CARRIED IN THE AIRPLANE AND AVAILABLE TO THE PILOT AT ALL TIMES.  \nRevision 1 U.S. i  \nINTRODUCTION CESSNA  \nMODEL 208B G1000  \nPERFORMANCE-SPECIFICATIONS  \nCARGO VERSION  \n*SPEED (KTAS):  \nMaximum Cruise at 10,000 Feet   175 Knots  \nMaximum 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.  \nMax Cruise at 10,000 Feet   Range 862 NM  \n  Time-5.1 Hours Max Cruise at 18,000 Feet   Range-1044 NM  \n  Time-6.6 Hours Max Range at 10,000 Feet   Range-963 NM  \n  Time-6.5 Hours Max Range at 18,000 Feet   Range-1076 NM  \n  Time-7.0 Hours RATE-OF-CLIMB AT SEA LEVEL   925 FPM SERVICE CEILING   22,800 Feet MAXIMUM OPERATING ALTITUDE   25,000 Feet  \nTAKEOFF PERFORMANCE:  \nGround Roll   1405 Feet  \nTotal Distance Over 50 Foot Obstacle   2500 Feet LANDING PERFORMANCE:  \nGround Roll   915 Feet  \nTotal Distance Over 50 Foot Obstacle   1740 Feet STALL SPEED (KCAS):  \nFlaps Up, Idle Power   78 Knots  \nFlaps Full, Idle Power   61 Knots MAXIMUM WEIGHT:  \nRamp   8785 Pounds Takeoff   8750 Pounds Landing   8500 Pounds STANDARD EMPTY WEIGHT   4680 Pounds  \nMaximum USEFUL LOAD   4105 Pounds *Speeds are based on mid-cruise weight.  \n(Continued Next Page)  \nii U.S. Revision 1  \nCESSNA INTRODUCTION  \nMODEL 208B G1000  \nPERFORMANCE-SPECIFICATIONS  \nCARGO VERSION (Continued)  \nWING 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  \nFree Turbine Flat Rated at 675 Shaft Horsepower PROPELLER:  \nMcCauley 3-bladed, Constant Speed, Full Feathering, Reversible Propeller  \nDiameter   106 Inches  \nNOTE  \nThe above performance figures are based on indicated weights, standard atmospheric conditions, level, hardsurfaced 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.  \nRevision 1 U.S. iii  \nINTRODUCTION CESSNA  \nMODEL 208B G1000  \nPERFORMANCE-SPECIFICATIONS  \nPASSENGER VERSION  \n* SPEED (KTAS):  \nMaximum Cruise at 10,000 Feet   184 Knots  \nMaximum 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.  \nMax Cruise at 10,000 Feet   Range-907 NM  \n  Time-5.1 Hours Max Cruise at 18,000 Feet   Range-1109 NM  \n  Time-6.6 Hours Max Range at 10,000 Feet   Range-1026 NM  \n  Time-6.6 Hours Max Range at 18,000 Feet   Range-1163 NM  \n  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:  \nGround Roll   1365 Feet  \nTotal Distance Over 50 Foot Obstacle   2420 Feet LANDING PERFORMANCE:  \nGround Roll   950 Feet  \nTotal Distance Over 50 Foot Obstacle   1795 Feet STALL SPEED (KCAS):  \nFlaps Up, Idle Power   78 Knots  \nFlaps Full, Idle Power   61 Knots MAXIMUM WEIGHT:  \nRamp   8785 Pounds Takeoff   8750 Pounds Landing   8500 Pounds STANDARD EMPTY WEIGHT   4511 Pounds  \nMaximum USEFUL LOAD   4274 Pounds *Speeds are based on mid-cruise weight.  \n(Continued Next Page)  \niv U.S. Revision 1  \nCESSNA INTRODUCTION  \nMODEL 208B G1000  \nPERFORMANCE-SPECIFICATIONS  \nPAS","cbCaihTNfbBayef2","https://ap.wps.com/l/cbCaihTNfbBayef2","pdf",18344268,536,"English","# Performance-Specifications\n## Cargo Version\n## Passenger Version\n## Warnings, Cautions, and Notes","[{\"question\":\"What does the manual caution about using this information as a substitute?\",\"answer\":\"It states that the information manual is an exact duplicate at issuance, is not kept current, and cannot be used as a substitute for the official Pilot’s Operating Handbook and FAA approved Airplane Flight Manual.\"},{\"question\":\"What cruise speeds and ranges are given for the cargo version?\",\"answer\":\"The cargo version provides maximum cruise speeds at 10,000 and 20,000 feet, along with range values and time estimates for those cruise profiles.\"},{\"question\":\"How are the performance numbers qualified in the manual?\",\"answer\":\"It notes the figures are based on indicated weights, standard atmospheric conditions, level hard-surfaced dry runways, and no wind, and they are calculated from flight tests under documented conditions.\"}]","CESSNA INTRODUCTION - MODEL 208B G1000 - Performance Specifications - Cargo Version | PDF",1792882421,1351]