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General| Manufacturer | Cessna |
|---|---|
| Model | T206H |
| Engine | Lycoming TIO-540-AJ1A |
| Horsepower | 310 hp |
| Seating Capacity | 6 |
| Category | Single-engine piston |
| Range | 703 nautical miles |
| Service Ceiling | 25, 000 feet (7, 620 meters) |
| Fuel Capacity | 87 gallons |
| Max Takeoff Weight | 3, 600 pounds |
| Wingspan | 36 feet 0 inches |
| Length | 28 feet 3 inches |
| Height | 9 feet 4 inches |
Details aircraft performance parameters including speed, climb, and weight.
Provides key aircraft specifications including weight and loading limits.
Details wing loading and power loading for performance calculations.
Outlines critical airspeed limitations and their operational significance.
Explains color-coded markings on the airspeed indicator and their meaning.
Specifies maximum certificated weights for ramp, takeoff, and landing.
Defines the acceptable forward and aft center of gravity ranges.
Details the flight load factors for different flap configurations.
Lists key airspeeds for emergency situations like maneuvering and gliding.
Provides procedures for engine failure, including restart and emergency descent.
Offers expanded guidance for specific emergency scenarios.
Details recommended airspeeds for normal flight operations and specific configurations.
Specifies speeds for optimal climb rate and angle with flaps up.
Identifies the recommended speed for flying in turbulent air.
Covers normal and short field takeoff techniques and speeds.
Provides additional details and procedures for normal flight operations.
Describes flap settings for takeoff and their impact on performance.
States the certificated takeoff noise level and its regulatory basis.
Lists stall speeds under various flap and bank angle conditions.
Presents stall speeds for the most rearward center of gravity.
Presents stall speeds for the most forward center of gravity.
Provides takeoff distances for short fields under various conditions.
Details the maximum rate of climb performance at different altitudes.
Shows time, fuel, and distance required for climb at max rate.
Details time, fuel, and distance for normal climb at 95 KIAS.
Cruise performance data at 2000 feet pressure altitude.
Cruise performance data at 4000 feet pressure altitude.
Cruise performance data at 6000 feet pressure altitude.
Cruise performance data at 8000 feet pressure altitude.
Cruise performance data at 10,000 feet pressure altitude.
Cruise performance data at 12,000 feet pressure altitude.
Cruise performance data at 14,000 feet pressure altitude.
Cruise performance data at 16,000 feet pressure altitude.
Cruise performance data at 18,000 feet pressure altitude.
Cruise performance data at 20,000 feet pressure altitude.
Cruise performance data at 22,000 feet pressure altitude.
Cruise performance data at 24,000 feet pressure altitude.
Range profile chart for 64 gallons usable fuel with 45 min reserve.
Range profile chart for 87 gallons usable fuel with 45 min reserve.
Endurance profile chart for 64 gallons usable fuel with 45 min reserve.
Endurance profile chart for 87 gallons usable fuel with 45 min reserve.
Graphical representation of the aircraft's center of gravity moment envelope.
Graphical representation of the aircraft's center of gravity limits.
