Cessna 206: Definition, Specifications, Difference, Interior

Jim Goodrich • Reading time: 27 min

cessna 206

The Cessna 206 is a single-engine, high-wing aircraft designed for utility and versatility in various operational roles. The Cessna 206 incorporates specifications: engine performance, flight range, and wing dimensions that define its capabilities. Pilots and operators focus on the Cessna 206's cargo capacity, seating arrangements, and interior configurations for optimal functionality. The cockpit design ensures efficient control during takeoff and flight while facilitating potential conversions for specific missions. Understand the Cessna 206's model variations, performance metrics, and dimensional characteristics to evaluate its adaptability and operational efficiency.

The Cessna 206 measures 28 feet 3 inches (8.61 meters) in length, 9 feet 4 inches (2.84 meters) in height, and features a wingspan of 36 feet (10.97 meters). Equipped with a Lycoming IO-540-AC1A5 piston engine producing 300 horsepower, the aircraft achieves a maximum speed of 142 knots and a normal cruise speed of 128 knots. The service ceiling reaches 15,700 feet (4,785 meters) with a climb rate of 920 to 988 feet per minute (280 to 301 meters per minute). The aircraft offers a normal range of 594 nautical miles and a maximum range of 721 nautical miles under optimal conditions. The cabin provides a volume of 102 cubic feet with an internal baggage capacity of 11 cubic feet.

The Cessna 206 accommodates one pilot and five passengers, while the Cessna 207 expands seating to six passengers. Both models achieve a maximum speed of 174 mph (280 km/h) but differ in cabin layout and ease of access. The Cessna 207 features dual front doors for augmented passenger and cargo loading efficiency. Variations in service ceiling and climb rates result from increased weight and dimensions in the Cessna 207 compared to the Cessna 206.

The Cessna 206 cockpit includes an instrument panel, avionics system, communication and navigation radios, control systems, and switch panels. The attitude indicator displays the aircraft's orientation relative to the horizon, while the altimeter provides accurate altitude readings important for maintaining safe flight levels. The airspeed indicator measures speed in knots, and the vertical speed indicator shows climb or descent rates in feet per minute. The gauge cluster integrates fuel quantity indicators, oil pressure and temperature gauges, and electrical system monitors. The avionics system incorporates GPS receivers, VHF navigation radios, and ADF receivers to enhance route management and assure precise tracking.

Cessna 206 aircraft are available for purchase through online marketplaces like Trade-A-Plane, Controller.com, and Barnstormers.com. Prices range from $180,000 for older models to $598,888 for newer variants. Aircraft dealerships located in the United States, Canada, Australia, and South Africa offer both new and used models, including turbocharged variants. Listings include detailed specifications covering seating capacity, engine type, and additional modifications. Aviation classified ads and auctions provide additional avenues for acquiring the aircraft.

What is the Cessna 206?

The Cessna 206 is a versatile and robust single-engine aircraft with fixed landing gear, often used in both personal and commercial aviation for its spacious cabin, stable handling, and utility as a reliable hauler. The Cessna 206 measures 28 ft 3 in (8.61 m) in length, 9 ft 4 in (2.84 m) in height, and 36 ft 0 in (10.97 m) in wingspan, offering typical ground clearance for a high-wing aircraft. The aircraft provides a cabin volume of 102 cu ft and internal baggage capacity of 11 cu ft, making it a spacious hauler for both passengers and cargo. Equipped with a Lycoming IO-540-AC1A5 piston engine delivering 300 horsepower, the Cessna 206 achieves a max speed of 142 knots and a normal cruise speed of around 128 knots. The Cessna 206 reaches a service ceiling of 15,700 ft (4,785 m) and offers a normal range of about 594 nm (1,100 km) with a max range of up to 721 nm (1,335 km). Large windows and a high wing configuration enhance visibility, increasing its appeal for pilots who value clear views during flight.

cessna 206 interior

The Cessna 206 plane excels as a multi-purpose aircraft, serving roles in bush flying, cargo transport, and passenger carriage. The bush plane rough-field capability allows operations from unpaved or short runways, making it ideal for remote areas. Equipped with a Lycoming IO-540-AC1A engine producing 300 horsepower, the aircraft achieves a cruise speed of 142 knots and a range of up to 840 nautical miles under optimal conditions. The Cessna 206 high-wing design enhances stability and visibility, essential for low-altitude maneuvers and landings in challenging environments. Pilots value the STOL (Short Takeoff and Landing) aircraft short runway performance, enabling takeoffs within 675 feet (205.74 meters) and access to rugged terrains.

The Cessna 206 utility is evident in its spacious cabin layout, offering seating for one pilot and five passengers while maintaining internal baggage capacity of 11 cubic feet. The cargo capacity reaches up to 1,441 pounds (653.7 kilograms) in some models, accommodating both people and equipment efficiently. The high-wing configuration ensures excellent downward visibility, benefiting aerial photography and scenic tours. The Lycoming engine includes variants like the TIO-540-AJ1A in the T206 Turbo Stationair model, delivering 310 horsepower for boosted performance at higher altitudes. The service ceiling of 15,700 feet (4,785 meters) and climb rate of 920 to 988 feet per minute (280 to 301 meters per minute) further demonstrate its versatility across diverse missions.

The Cessna 206 specifications highlight dimensions including a length of 28 feet 3 inches (8.61 meters), wingspan of 36 feet (10.97 meters), and height of 9 feet 3 inches (2.82 meters), contributing to its compact yet functional design. The Cessna 206 bush plane reputation stems from robust construction built for demanding environments, appealing to pilots requiring reliability and adaptability. General aviation aircraft civil aviation operators choose the Cessna 206 due to its predictable handling and ease of maintenance. The Cessna aircraft company manufacturer has designed this model to balance durability with flexibility, assuring suitability for both recreational and commercial purposes. Pilots commend the Cessna 206 flight characteristics, citing stability and responsive controls even during turbulent conditions.



What are the specifications of the Cessna 206?

The specifications of the Cessna 206 are given in the table below.

Specification

Details

Length

28 feet 3 inches (8.61 meters) (8.61 meters)

Wingspan

36 feet 0 inches (10.97 meters)

Height

9 feet 4 inches (284 centimeters) / 9 feet 3+1/2 inches (283 centimeters)

Empty Weight

2,176 pounds (987 kilograms)

Maximum Takeoff Weight

3,600 pounds (1,633 kilograms)

Fuel Capacity

87 gallons (329 liters)

Range

840 miles (1,350 kilometers) with reserves

Service Ceiling

15,700 feet (4,800 meters)

Rate of Climb

988 feet per minute (301.1 meters per minute) (5.02 meters per second)

Cruise Speed

163 mph (262 km/h) at 1890 meters with 75% power

Maximum Speed

174 mph (280 km/h) at sea level

Takeoff Distance

1,863 feet (568 meters)

Landing Distance

2,358 feet (719 meters)

Engine Options

Lycoming IO-540-AC1A (300 hp) or TIO-540-AJ1A (310 hp)

Propeller

3-bladed McCauley metal constant-speed propeller

The height measurement varies , standing at 9 feet 4 inches (2.84 meters) for most models and 9 feet 3+1⁄2 inches (2.83 meters) for the 206H Stationair. These specifications define the Cessna 206 dimensions and operational limits. These figures highlight the Cessna 206 cruise efficiency and Cessna 206 top performance capabilities. The fuel capacity unit and distances are expressed in gallons, feet, and meters to assure clarity for pilots and operators managing Cessna 206 fuel and operational planning. These features enhance the Cessna 206 speed and versatility across various missions.

What is the performance of the Cessna 206?

The performance of the Cessna 206 is given in the table below.

Parameter

Value

Maximum Cruise Speed (mph/km/h)

174 mph (280 km/h) / 280 km/h (174 mph)

Normal Cruise Speed (knots)

147 knots

Economy Cruise Speed (knots)

117 knots

Turbo Stationair Max Cruise (knots)

161 knots

Service Ceiling (feet/meters)

15,700 ft (4,785 m) / 4,785 m (15,700 ft)

Climb Rate (ft/min / m/min)

988 ft/min (301.1 m/min) / 301.1 m/min (988 ft/min)

Operational Range (miles/km)

840 mi (1,352 km) / 1,352 km (840 mi)

Fuel Capacity (gallons/liters)

90 gal (340.69 L) / 340.69 L (90 gal)

Takeoff Distance (feet/meters)

675 ft (205.74 m) / 205.74 m (675 ft)

Stall Speed (mph/knots)

63 mph / 55 knots (101.4 km/h / 101.86 km/h) (flaps down)

Engine Type (Standard Model)

Lycoming IO-540-AC1A

Engine Power (Standard Model)

300 hp

Engine Type (Turbo Stationair)

Lycoming TIO-540-AJ1A

Engine Power (Turbo Stationair)

310 hp

Aircraft Length (feet/meters)

28 ft 3 in (8.61 m) / 8.61 m (28 ft 3 in)

Wingspan (feet/meters)

36 ft (10.97 m) / 10.97 m (36 ft)

Height (feet/meters)

9 ft 4 in (2.84 m) / 2.84 m (9 ft 4 in)

Average Fuel Consumption ($/hr)

$220.95

Range with Reserve (miles/km)

840 mi (1,351.86 km) / 1,351.86 km (840 mi)

Range with Specific Config (NM)

563 NM

At 1890 meters under 75% power, the aircraft cruises efficiently at 163 mph (262 km/h). The climb rate varies between 920 ft/min (280.4 m/min) and 988 ft/min (301.1 m/min) feet per minute depending on load and environmental conditions. Performance under different load configurations directly impacts the climb rate, while altitude conditions influence overall speed capabilities. Fuel burn rate and weight distribution affect the total range, making careful planning important for maximizing performance. Landing roll distance requires precise calculation to provide safe deceleration on the runway. Weight and configuration influence both takeoff and landing performance, with stall speed recorded at 63 mph (55 knots) when flaps are down. Environmental factors like temperature and altitude play a crucial role in determining safe operating parameters. The adaptability of the Cessna 206 extends to varying weather conditions and altitudes, with a service ceiling of 15,700 feet (4,785 meters) defining its atmospheric performance limits. The Lycoming TIO-540-AJ1A engine in the Turbo Stationair model produces 310 hp, while the standard model features the Lycoming IO-540-AC1A engine generating 300 horsepower. These engines contribute to robust performance to provide reliability across diverse operational scenarios.

What is the engine specification of the Cessna 206?

The engine specification of the Cessna 206 is given in the table below.

Engine Model

Configuration

Displacement (cu in)

Horsepower (HP)

Additional Features

Continental IO-520

Horizontally Opposed 6-Cylinder

520

285 (Naturally Aspirated)

Fuel Injection

Continental TSIO-520-A

Horizontally Opposed 6-Cylinder

520

285

Turbocharged, Fuel Injection

Continental TSIO-520-M

Horizontally Opposed 6-Cylinder

520

310

Turbocharged, Fuel Injection

Lycoming IO-540-AC1A5

Horizontally Opposed 6-Cylinder

540

300

Naturally Aspirated

Lycoming TIO-540-AJ1A

Horizontally Opposed 6-Cylinder

540

310

Turbocharged, Fuel Injection

This engine type ensures consistent power delivery across diverse flight conditions. Fuel injection systems in the Cessna 206 engine model are essential in optimizing performance. Engine displacement and fuel metering systems directly influence operational flexibility. The Cessna 206 is equipped with engine configurations customized to specific mission requirements. Naturally aspirated and turbocharged engine options provide versatility for the Cessna 206. The Continental TSIO-520 series powers multiple variants, offering engine horsepower ratings of 285 hp, 300 hp, and 310 hp. The Lycoming IO-540 engine type delivers 300 hp in naturally aspirated form, while the Lycoming TIO-540-AJ1A achieves 310 hp with turbocharging. Engine type selection depends on operational needs, including payload capacity and altitude performance. The Cessna 206 is designed to adapt to both personal and commercial aviation demands.

The engine specification of the Cessna 206 includes options including the Continental TSIO-520 and Lycoming IO-540 series. Turbocharging and fuel injection enhance engine efficiency across various configurations. Engine options include naturally aspirated and turbocharged variants to suit operational needs. Horsepower ratings range from 285 HP to 310 HP depending on the installed engine model.

What are the differences between the Cessna 206 and 207?

Differences between the Cessna 206 and 207 are explained in the table below.

Feature

Cessna 206

Cessna 207

Seating Capacity

5 passengers

6 passengers

Front Passenger Doors

Single door

Dual doors

Cabin Width

43 inches (109.22 cm)

Slightly wider

Cabin Height

4 ft 2 in (1.27 m)

Comparable to Cessna 206

Cabin Length

10 ft 7 in (3.23 m) (10.58 ft)

Longer

Payload Capacity

1,359 lbs (616 kg)

Reduced due to larger size

Engine Model

Textron Lycoming IO-540-AC1A5

Textron Lycoming IO-520-F

Engine Power

300 horsepower

300 horsepower

Maximum Speed

174 mph (280 km/h)

174 mph (280 km/h)

Service Ceiling

Higher

Lower due to increased weight

Rate of Climb

Higher

Lower

Operational Preference

Rugged utility missions

Comfort, stability, and ease

Accessibility

Single-door access

Enhanced with dual front doors

The Cessna 207 accommodates six passengers compared to the five-passenger capacity of the Cessna 206. Both aircraft achieve a maximum speed of 174 mph (280 km/h) and share comparable performance metrics, though the Cessna 207 exhibits variations in service ceiling and rate of climb due to increased weight and dimensions. Accessibility differs, as the dual front doors of the Cessna 207 enhance passenger and cargo loading efficiency.

The differences between the Cessna 206 and Cessna 207 include variations in seating capacity, cabin layout, and ease of access. The Cessna 207 provides more internal space, improving comfort and cargo capacity. Both aircraft share similar engine configurations, maintaining comparable performance metrics. The Cessna 206 achieves a maximum speed of 174 mph (280 km/h), matching the capabilities of the Cessna 207.

What are the differences between the Cessna 206 and 210?

Differences between the Cessna 206 and 210 are explained in the table below.

Criteria

Cessna 206

Cessna 210

Landing Gear

Fixed landing gear

Retractable landing gear

Cruise Speed

140–150 mph (225.3–241.4 km/h)

180 mph (289.7 km/h)

Useful Load Capacity

Higher useful load capacity

Lower useful load capacity

Engine

Continental IO-520 (300 hp)

Continental IO-520 (300 hp)

Turbocharged Variants

Available

Available

Maximum Takeoff Weight

3,600 lbs (1,632.93 kg)

Varies by model

Wing Design

Strutted wing

Strutless wing (later models)

Aerodynamic Efficiency

Moderate

Higher (due to strutless wing)

Maintenance Complexity

Lower

Higher (retractable gear)

Seating Capacity

Up to 6 passengers

Up to 6 passengers

Cabin Space

Roomier cabin

Slightly reduced cabin space

Operational Focus

Utility and versatility

Speed and performance

The engine configurations of the Cessna 206 and Cessna 210 exhibit similarities but differ in power output and design. Turbocharged variants of both models enhance performance at higher altitudes, with the Cessna 210 achieving higher cruise speeds due to its retractable landing gear configuration. The cruise speeds and overall performance metrics highlight the trade-offs between the two models. The Cessna 210 achieves cruise speeds up to 180 mph (289.7 km/h), surpassing the Cessna 206’s range of 140 to 150 mph (225.3 to 241.4 km/h). This performance advantage makes the Cessna 210 suitable for pilots prioritizing speed. The Cessna 206 demonstrates a higher useful load capacity, exceeding that of the Cessna 210, making it more versatile for cargo and passenger transport. This structural change introduces increased complexity and maintenance requirements, including reinforcements to the fuselage. The Cessna 206’s simpler fixed-gear design focuses on utility and flexibility, allowing effective operation in various environments without additional structural modifications. Aircraft specifications, including dimensional and performance metrics, reveal similar overall dimensions, with the Cessna 210 offering higher cruise speeds and the Cessna 206 providing superior payload capacity. These differences cater to distinct operational needs within general aviation.

The differences between the Cessna 206 and Cessna 210 include variations in landing gear configuration, useful load capacity, cruise speeds, and structural design. Later models of the Cessna 210 feature a strutless wing design, augmenting aerodynamic efficiency but increasing structural complexity.

What is the difference between the Cessna 206 and 172?

Differences between the Cessna 206 and 172 are explained in the table below.

Category

Cessna 206

Cessna 172

Engine

Continental IO-520

Lycoming IO-360

Engine Power (HP)

285 HP

160 to 180 HP

Fuel Consumption (GPH)

13 (49.21 to 53.01 liters) to 14 (53.01 to 56.78 liters) gallons/hour

7 to 10 gallons/hour (26.5 to 37.9 liters/hour)

Cruise Speed (mph)

140 to 150 mph (225 to 241 km/h)

120 to 140 mph (193 to 225 km/h)

Cruise Speed (km/h)

225.3 to 241.4 km/h (140 to 150 mph)

193.1 (120 to 139.9) to 225.3 (140 to 161.7) km/h

Max Takeoff Weight (lbs)

3,600 lbs (1,632.93 kg)

2,550 lbs (1,157 kg)

Max Takeoff Weight (kg)

1,632.93 kg (3,598.04 lbs)

1,156.66 kg (2,549.96 lbs)

Payload Capacity

Higher payload capacity

Lower payload capacity

Cabin Configuration

Larger cabin, removable seats for cargo flexibility

Compact trainer-oriented design

Operational Role

Utility, cargo, backcountry missions

Personal flying, flight training

Range

Longer range due to higher fuel capacity and engine performance

Shorter range; efficient for training and personal use

Cruise speeds of the Cessna 206 range from 140 mph (225.3 km/h) to 150 mph (241.4 km/h), surpassing the Cessna 172's 120 mph (193.1 km/h) to 140 mph (225.3 km/h). Structural differences highlight the Cessna 206 cabin configuration layout, featuring utility-focused designs for cargo flexibility. Engine specifications power varies between the two aircraft. The Cessna 206 relies on a Continental IO-520 engine producing 285 HP, whereas the Cessna 172 uses a Lycoming IO-360 engine rated at 160 to 180 HP. Fuel consumption rates differ, with the Cessna 206 burning 13 (49.2 liters) to 14 (53 liters) gallons per hour compared to the Cessna 172's efficient rate of 7 (26.5 liters) to 10 (37.9 liters) gallons per hour. These differences underscore the Cessna 206 performance focus versus the Cessna 172's emphasis on economy and simplicity.

The difference between the Cessna 206 and Cessna 172 lies in their design, performance, and roles, with the Cessna 206 featuring a larger size, higher payload capacity, and utility-focused missions compared to the smaller, more fuel-efficient Cessna 172 suited for training and personal flying.

What is inside a Cessna 206 cockpit?

Inside a Cessna 206 cockpit is an instrument panel, avionics system, communication radios, navigation radios, control systems, switch panels, and cabin seating. The attitude indicator displays the aircraft's orientation with respect to the horizon, assuring precise control during flight. The altimeter provides accurate altitude readings above sea level, important for maintaining safe flight levels. The airspeed indicator measures the aircraft's speed in knots, enabling optimal performance and fuel efficiency. The vertical speed indicator shows climb or descent rates in feet per minute, amplifying situational awareness. The gauge cluster integrates fuel quantity indicators, oil pressure and temperature gauges, and electrical system monitors for comprehensive system oversight.

The avionics navigation system integrates GPS receivers, VHF navigation radios, and ADF receivers to enhance route management. The avionics system autopilot stabilizes the aircraft during flight, reducing pilot workload. The avionics system interface consolidates navigation, communication, and other systems into a unified display. Communication radios and transceivers enable two-way voice interaction with air traffic control and other aircraft. Communication radios audio control manages audio inputs from various sources. Navigation radios VHF receiver processes signals from VOR stations for precise tracking. Navigation radios GPS receiver provides accurate position data for navigation. Navigation radios ADF receiver detects signals from non-directional beacons.

Control yoke steering allows directional adjustments on the ground, while control yoke pitch and roll control modifies the aircraft's angle of attack and bank angle. Throttle quadrant throttle lever regulates engine power output, throttle quadrant mixture control adjusts the fuel-air ratio for optimal engine performance, while throttle quadrant propeller control alters propeller pitch to suit flight conditions. Flap lever control extends or retracts flaps as needed, and flap lever indicator displays the current flap position. Pedal assemblies rudder pedals provide directional control in the air and on the ground, while pedal assemblies brake pedals activate wheel brakes for stopping.

Overhead switch panel system switches manage electrical and mechanical systems. Circuit controls regulate individual circuits for operational safety. Circuit breaker panel switches protect against electrical overloads and safeguard system damage during faults. Engine start panel ignition switch activates the engine's ignition system, and engages the starter motor. Engine start panel engine start button initiates the engine startup sequence.

Cabin lighting control switch adjusts overall cockpit illumination, while dimming control modifies light intensity for comfort, maintaining visibility during night operations. Seating pilot seat and seating copilot seat are designed with ergonomic seating principles to reduce fatigue during extended flights.



What materials are used in the cabin of a Cessna 206?

The materials used in the cabin of a Cessna 206 include vinyl, leather, nylon carpeting, composite panels, and aluminum trim. Vinyl upholstery ensures ease of cleaning and resistance to wear and tear in high-traffic aircraft environments. Leather upholstery provides a premium finish with natural grain texture, and enhances the aesthetic appeal of the cabin in upgraded Cessna 206 models. Leather natural grain offers a soft seating experience, reducing fatigue during long flights.Nylon carpeting provides sound insulation to reduce noise levels within the cabin. Composite panels reduce the overall weight of the Cessna 206 to enhance aircraft performance. Aluminum trim maintains its condition over time due to its corrosion-resistant properties.


Carpeting textile material in the Cessna 206 consists of a durable nylon cut pile, selected for its resilience in heavy-use conditions. Carpeting sound insulation reduces noise levels within the cabin, creating quieter flying conditions. Composite panels’ lightweight structure contributes to reduced overall aircraft weight, enhancing performance. Composite panels impact resistance ensures passenger safety during turbulence or minor impacts. These panels maintain structural integrity while aiding fuel efficiency.

Aluminum trim metal alloy forms the interior framework, offering corrosion-resistant properties. Aluminum trim corrosion resistance ensures longevity, even in challenging environments. The trim retains its appearance and structural condition over extended periods. Aluminum components provide strength without adding excessive weight, endorsing the aircraft's operational efficiency.

Interior insulation thermal barrier regulates heat transfer, maintaining comfortable cabin temperatures. Interior insulation sound dampening minimizes external noise, augmenting the flying experience. Insulation reduces the need for additional heating or cooling systems, contributing to energy efficiency. The Cessna 206 cabin dimensions include a volume of 102 cubic feet, accommodating up to five passengers with ample space for baggage.



Is the Cessna 206 available as a taildragger?

No, the Cessna 206 is not available as a taildragger in a widely recognized or factory-produced version. The Cessna 206 features a tricycle landing gear configuration as its default setup. Factory-produced taildragger versions of the Cessna 206 do not exist. Discussions about converting the aircraft to a taildragger involve exploratory ideas rather than practical, certified modifications. Structural modifications for a tailwheel configuration require reinforcing the airframe and altering weight distribution. Obtaining a Supplemental Type Certificate ensures compliance with aviation safety standards.

Aftermarket tailwheel conversion kits exist for other Cessna models like the Cessna 172 and Cessna 182. These kits are not directly compatible with the Cessna 206 due to design differences and weight distribution variations. Custom aftermarket modifications enable taildragger conversions for the Cessna 206 but require pursuing necessary engineering, testing, and regulatory approvals. Structural reinforcements support the different loading conditions of a tailwheel configuration. Obtaining a Supplemental Type Certificate ensures compliance with aviation safety standards. The Federal Aviation Administration or equivalent bodies issue the STC for modifications.

Custom conversions of the Cessna 206 to a taildragger involve difficulties. Installation complexity and cost implications make such modifications less practical. Enthusiasts explore custom modifications for the Cessna 206 to a taildragger. These conversions remain theoretical and are not standard or widely performed. Factors like weight distribution, ground handling, and flight dynamics are necessary for taildragger conversions. Tailwheel conversion kit certification for safe installation is important to meet aviation authority requirements. The Cessna 206 version most seen in operation retains its original tricycle gear design.



What is the retraction mechanism of the Cessna 206 gear?

The retraction mechanism of the Cessna gear does not feature the Cessna 206 as it excludes retractable landing gear systems. The Cessna 206 incorporates a fixed landing gear configuration designed for stability during ground operations. Fixed landing gear remains extended at all times, providing consistent performance without the need for complicated retraction systems. Hydraulic and electrical components control actuation systems in retractable gear systems, but these mechanisms do not apply to the Cessna 206. Extended landing gear reduces maintenance requirements while assuring reliable operation in various conditions. Aerodynamic efficiency is sacrificed in favor of simplicity and durability in the Cessna 206 design.

Retractable landing gear systems in other aircraft rely on precise activation sequences and actuation control methods. Hydraulic cylinders serve as actuators in retractable gear systems, applying force to retract or extend landing gear during operation. Pilots activate gear selector valves to direct pressurized fluid, which routes to gear actuators during retraction mechanism activation sequence. Pressurized fluid from power packs drives actuators, pulling landing gear into gear wells while gear doors close tightly over gear wells for aerodynamic closure. Electrical switches and sensors monitor landing gear position to provide safe locking after retraction in landing gear retractable assembly.

Mechanical linkages and lever-and-pivot designs translate actuator motion into gear movement in retractable systems. Linkages connect gear doors to gear legs for smooth operation through pivots that reduce friction during retraction mechanism operation mode. Levers and pivots assure reliable gear retraction by converting linear actuator motion into rotational movement. Gear doors mechanically link to the landing gear, closing after retraction to enhance aerodynamic efficiency in gear doors aerodynamic closure. The Cessna 206 excludes such mechanisms, maintaining a fixed gear configuration for operational simplicity.

Aerodynamic trade-offs highlight the differences between retractable systems and the Cessna 206's design. Retractable gear systems reduce drag by closing gear doors over gear wells, developing aircraft performance. Aerodynamic efficiency results from this coverage, but complexity increases due to hydraulic and electrical components. The Cessna 206 sacrifices aerodynamic refinement for consistent performance, with extended landing gear providing stability during ground operations in Cessna 206 gear configuration. Fixed landing gear eliminates the need for gear doors and mechanical linkages, focusing on durability and reliability in various conditions.



What is the Cessna 206 seaplane?

The Cessna 206 seaplane is a versatile amphibious aircraft known for its ability to operate on both water and land, featuring a robust Lycoming IO-540 engine and a maximum range of about 840 miles (1352 kilometers). The Cessna 206 aircraft, known as the Stationair, serves both personal and commercial purposes with its adaptable design. Measuring 28 feet (8.53 meters) 3 inches (7.62 centimeters) in length and featuring a wingspan of 36 feet (10.97 meters), the plane accommodates various missions. Powered by a Lycoming IO-540 engine producing 300 hp (223.7 kW), the aircraft achieves a maximum speed of 174 mph (280 km/h) and a cruise speed of 163 mph (262.3 km/h). Equipped with amphibious floats, the Cessna 206 operates on water bodies like lakes, providing access to remote areas without conventional runways.

Seaplane conversion transforms the Cessna 206 into a versatile amphibious aircraft. The process involves installing seaplane floats using a float conversion conversion kit, which ensures structural integrity for water operations design. Certified installation guarantees that all modifications meet aviation standards while maintaining the aircraft's airworthiness. Seaplane floats consist of corrosion-resistant aluminum or composite materials, guaranteeing durability in both freshwater and salty environments. Float design focuses on providing substantial buoyancy and stability during water landing capability and takeoff performance. Amphibious adaptation integrates retractable landing gear, enabling seamless transitions between land and water operations.

Water landing capability enhances the Cessna 206 seaplane's operational versatility. Handling stability improves through the broad footprint and added lift provided by the floats. Water takeoff performance requires 25-30% shorter distances compared to land-based operations, with climb rates increasing by up to 20%. The aircraft achieves optimal performance in challenging marine conditions due to its robust construction and aerodynamic profile. Seaplane floats support a maximum weight capacity of 3,776 lbs (1,713 kg), while amphibious floats accommodate up to 4,000 lbs (1,814 kg). These features make the aircraft suitable for remote areas without conventional runways.

Pilots operating the Cessna 206 seaplane require specialized training to master water-specific skills. Handling characteristics differ from land-based aircraft, demanding proficiency in judging wave heights and managing crosswinds during water operations. Pilots focus on executing safe approach and departure procedures to assure reliable performance. The Cessna 206 seaplane pilot benefits from the aircraft's inherent stability, which enhances control during water landings and takeoffs. Adaptability for various missions, including cargo transport, passenger flights, and recreational flying, underscores the aircraft's utility in diverse environments. The integration of amphibious floats facilitates access to regions with limited infrastructure while retaining standard performance characteristics.



Where can I find a Cessna 206 for sale?

You can find a Cessna 206 for sale on online aviation marketplaces like Trade-A-Plane, Controller.com, and Barnstormers.com. Trade-A-Plane updates its listings daily, offering a variety of private seller options. Controller.com provides detailed listings with prices ranging from $180,000 to $598,888. Barnstormers.com includes amphibious models like the 1996 C206H priced at $520,000. AircraftForSale.com lists both older models, for instance, a 1965 P206 for $180,000, and newer ones like a 2006 T206H for $800,000. Search filters on these platforms allow users to refine results by price, location, and specific features.

Aircraft dealerships provide a reliable source for finding a Cessna 206 for sale. Aircraft dealerships inventory includes a mix of new and used models, the 1965 Cessna P206 priced at $155,000 and turbocharged variants. Authorized dealers certified by Cessna guarantee adherence to manufacturer standards, offering verified options for buyers. Dealerships are located in regions like the United States, Canada, Australia, and South Africa, enabling global accessibility. Listings from authorized dealers highlight key features, including seat configurations and turbo options, meeting specific buyer requirements.

Online aviation marketplaces listings offer extensive options for purchasing a Cessna 206. Trade-A-Plane updates its inventory daily, featuring 66 aircraft available for purchase with filtering options for price, location, and model type. Controller.com lists Cessna 206 aircraft with prices ranging from $180,000 for older models to $598,888 for newer variants. Barnstormers.com includes specialized models like the 1996 C206H Amphibian priced at $520,000. Online aviation marketplaces search filters allow users to refine results by price range, geographical location, and specific features including turbocharged engines or amphibious capabilities.

Used aircraft brokers maintain a diverse inventory of pre-owned Cessna 206 aircraft, including turbine-powered and turbocharged models. Brokers leverage their network spanning continents like Australia and South Africa to connect buyers with sellers. Expertise in evaluating aircraft condition ensures accurate valuation and guidance for buyers seeking a Cessna 206 occasion. Used aircraft brokers inventory includes detailed specifications about seating capacity, engine type, and additional modifications.

Aviation classified ads advertisements on platforms like Barnstormers.com and Trade-A-Plane.com provide direct access to sellers. Classified ads contact information facilitates communication with private sellers listing aircraft for sale. Listings include details about seat counts, turbo options, and other specifications. Aircraft auctions auction dates are scheduled periodically, offering opportunities for competitive bidding. Auction participation requires strategic planning, with bidding conducted either in person or online.



What is the price of a Cessna 206?

The price of a Cessna 206 depends on factors like age, condition, configuration, and model. Older models with high engine hours cost around $180,000. Well-maintained Cessna 206s with low hours and modern avionics command prices near $598,888. The average cost of a pre-owned Cessna 206H variant is $450,000. New models like the 2024 T206H Stationair list prices starting at $980,000.

Older Cessna 206 models with high engine hours cost around $180,000, appealing to buyers seeking budget-friendly options. Market assessments estimate values for older units in varying conditions at $210,187, reflecting factors as maintenance history and equipment levels. The average cost of a pre-owned Cessna 206H variant is $450,000, which includes mid-range engine hours and standard avionics packages. Well-maintained aircraft with low hours and modern avionics command prices near $598,888, showcasing the impact of condition and upgrades on valuation. Premium configurations like the Turbo Stationair HD reach costs of $750,000, upheld by advanced performance features and advanced systems. Brand new 2024 T206H Stationair models list starting prices at $980,000, while nearly zero-hour aircraft achieve values up to $1,295,000, driven by factory-fresh builds and cutting-edge technology.