CESSNA INTRODUCTION - MODEL 208B G1000 - Performance Specifications - Cargo Version

Oct 24, 2026

Cessna Model 208B G1000 performance specifications for the cargo version provide key operational limits and expected aircraft capability. It lists cruise speeds by altitude, corresponding range and time figures, climb rate at sea level, service ceiling, maximum operating altitude, and takeoff and landing performance including ground roll and 50-foot obstacle distances. 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.

LanguageEnglish

CategoryTechnology

FormatPDF

Pages536

Reading Time22 h 31 min

AccessFree to download

Performance-Specifications

Cargo Version

Passenger Version

Warnings, Cautions, and Notes

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, 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. 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 PAS

FAQs

What does the manual caution about using this information as a substitute?

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.

What cruise speeds and ranges are given for the cargo version?

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.

How are the performance numbers qualified in the manual?

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.

Oct 24, 2026

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