Cessna 310: Definition, Specifications, Features, Difference

Jim Goodrich • Reading time: 17 min

cessna 310 airplane
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Cessna 310 is a twin-engine piston aircraft designed for high-performance flight operations. The aircraft features a cockpit equipped with advanced instruments and controls for efficient operation. Cessna 310 includes specifications including wingspan, cabin dimensions, and weight that define its performance capabilities. The model provides seating arrangements and baggage capacity optimized for passenger comfort. Understand the Cessna 310's engine power, range, and takeoff requirements to evaluate its role in aviation.

The Cessna 310 operates with a twin-engine configuration featuring wing-mounted reciprocating piston engines. Early models utilize specific horsepower engines while later variants incorporate upgraded horsepower engines for greater performance. Wing-mounted engines contribute to aerodynamic efficiency and stability by minimizing drag and providing optimal airflow.

Differences between the Cessna 310 and the Cessna 340 include airframe design and cabin configuration. The Cessna 340 features a pressurized cabin and more higher-output turbocharged engines compared to the non-pressurized cabin of the Cessna 310. Structural modifications in the Cessna 340 enhance suitability for long-distance flights at higher altitudes. Instrument panels in both models are configured for specific operational requirements but differ in complexity due to technological advancements.

To locate a Cessna 310 for sale, specialized sales platforms provide listings with varying prices and detailed advertisements. Dealerships offer verified inventory with certification guarantees transparency regarding aircraft history and condition. Brokerages connect buyers with experienced brokers familiar with market dynamics. Advanced search filters allow refinement based on specific criteria, including maintenance history and price fluctuations over time. Auction schedules provide opportunities for competitive bidding through real-time participation.

What is the Cessna 310?

The Cessna 310 is an iconic American twin-engine, low-wing monoplane aircraft produced from 1954 to 1980, known for its versatility, reliability, and distinctive design. Cessna airplane was, established as the first post-World War II twin-engine production model in its lineup. The Cessna 310 features a four-to-six-seat configuration, with later variants powered by 285-hp Continental IO-520-MB engines for boosted performance. Pilots achieve a maximum speed of 383 km/h (238 miles/h) and a range of 1,630 km (1,013 miles), supported by retractable tricycle landing gear and distinctive tip tanks. Aviation enthusiasts recognize the Cessna 310 for its sleek, aerodynamic low-wing design and exceptional reliability in cross-country travel. The aircraft's service ceiling reaches 19,750 feet (5,999 meters), guaranteeing efficient operations under diverse conditions.

Cessna 310 Interior

The Cessna 310 features a low-wing monoplane design with a twin-engine configuration for better stability and performance. The aircraft flying machine incorporates a four-to-six-seat cabin layout, offering versatility for various missions. Retractable tricycle landing gear ensures smooth ground handling, while distinctive tip tanks increase fuel capacity and aerodynamic efficiency. These design elements contribute to the Cessna 310's reputation as a reliable and versatile aircraft in the general aviation aviation sector.

Later Cessna 310 models are equipped with Continental IO-520-MB engines, each delivering 285 horsepower, enabling a maximum speed of 207 knots ( 238 mph). The Cessna 310 range extends up to 900 nautical miles (1,666.8 kilometers), with a service ceiling of 19,750 feet (6,019.8 meters). Pilots value the Cessna 310 for its cross-country travel efficiency and consistent performance under diverse conditions. Aviation enthusiasts recognize the Cessna 310 for its innovative dual-engine configuration and adaptability. The aircraft's enduring legacy reflects its impact on both private and commercial aviation sectors.

The Cessna 310 serves applications in private, corporate, and utility aviation, catering to a wide range of operational needs. Its spacious cabin accommodates up to six passengers, making it ideal for family trips or business travel. Pilots appreciate the Cessna 310's responsive handling and robust engine-out performance, with a single-engine service ceiling of up to 7,500 feet (2,286 meters). Fuel burn averages 25 gallons (94.63 liters) per hour at cruise for efficient operations. The Cessna 310 remains a staple in modern aviation contexts due to its balance of speed, comfort, and reliability.



What are the specifications of the Cessna 310?

The specifications of the Cessna 310 are given in the table below.

Specification

Value

Wingspan

36 feet 9 inches (11.2 meters) (36 feet 9 inches)

Length

32 feet (9.75 meters)

Height

10 feet 7 inches (3.23 meters) (323 centimeters)

Maximum Takeoff Weight

5,500 pounds (2,495 kilograms)

Empty Weight

3,358 pounds (1,523 kilograms)

Useful Load

2,163 pounds (981 kilograms)

Fuel Capacity (Standard)

102 gallons (386 liters)

Fuel Capacity (Optional)

Up to 120 gallons (454 liters)

Engine Type

Twin Continental TSIO-520-MB

Engine Power (Each)

285 horsepower

Passenger Capacity

Up to 5 passengers + 1 pilot

Normal Cruise Speed

188 knots

Range (Full Fuel Conditions)

725 nautical miles

These proportions enhance aerodynamic efficiency and allow for optimal performance during takeoff and landing. The weight specifications: max takeoff weight is set at 5,500 pounds (2,495 kg), with an empty weight of 3,358 pounds (1,523 kg). This balance between weight specifications, empty weight and payload supports extended operational flexibility. The TSIO-520 engines generate 285 horsepower each, enabling reliable twin engine performance. The cabin design prioritizes functionality, offering adequate space for comfort during flights.

What is the performance of the Cessna 310?

The performance of the Cessna 310 is given in the table below.

Performance Metric

Standard Models (260 hp)

TSIO-520 Engines (285 hp)

Turbocharged Variants

Maximum Speed

220 mph (354.064 km/h)

220 mph (354.064 km/h)

220 mph (354.064 km/h)

Cruise Speed

186 knots (344.472 km/h)

Exceeds 190 knots (351.88 km/h)

Exceeds 190 knots (351.88 km/h)

Range

Up to 1,000 miles (1,609 km)

Up to 1,000 miles (1,609 km)

Up to 1,000 miles (1,609 km)

Service Ceiling

20,000 feet (6,096 meters)

20,000 feet (6,096 meters)

20,000 feet (6,096 meters)

Rate of Climb

1,600 ft/min (487.68 m/min)

1,600 ft/min (487.68 m/min)

1,495 ft/min (455.68 m) (455.68 m/min)

Fuel Consumption at 70% Power

25 gallons/hr (94.63 liters/hr)

29 gallons/hr (110 liters/hr) (110 liters/hr) (29 gallons/hr)

Enhanced efficiency at altitude

Engine Power Output

260 hp (194 kW)

285 hp (213 kW)

285 hp (213 kW)

Optimal Altitude for Efficiency

7,500-10,000 feet (2,286-3,048 m)

7,500-10,000 feet (2,286-3,048 m)

Higher altitudes improve efficiency

The cruise speed of the Cessna 310 varies depending on engine configurations and power settings: models equipped with 240-hp engines achieve a cruise speed of 183 knots, while those with 260-hp engines reach 186 knots. The Cessna 310 with TSIO-520 engines producing 285 horsepower exceeds 190 knots at optimal settings. The range flight distance extends up to 1,000 miles (1,609 kilometers) or 870 nautical miles under standard conditions. Fuel efficiency improves at higher altitudes, around 7,500 (2,286 meters) to 10,000 (3,048 meters) feet, where fuel burn rates are 25 (94.63 liters) gallons per hour for 240 (179.1 kilowatts)-hp engines and 29 (110 liters) gallons per hour for 285 (212.6 kilowatts)-hp engines at 70% power. Takeoff and landing distances of the Cessna 310 depend on factors: weight, runway surface, and environmental conditions. The rate of climb vertical ascent exceeds 1,600 feet (487.68 meters) per minute for most models, with the Q model achieving 1,495 feet (455.68 meters) per minute under specific conditions. Turbocharged variants using TSIO-520 engines demonstrate increased climb performance at higher altitudes. The service ceiling maximum altitude is 20,000 feet (6,100 meters), providing operational flexibility in diverse scenarios. Fuel consumption rates of the Cessna 310 vary based on engine types and flight profiles. At 70% power and 7,500 feet (2,286 meters) altitude, models with 240-hp (179-kW) engines consume 25 gallons (95 liters) per hour, while those with 285-hp (213-kW) engines require 29 gallons (110 liters) per hour. Pilots optimize fuel efficiency by adjusting power settings and altitude during long-distance travel. The design of the Cessna 310 prioritizes efficient cruising over pure speed, enabling extended range endurance. Performance metrics of the Cessna 310 change with altitude and weather conditions. Higher altitudes optimizefuel efficiency due to reduced air resistance, while adverse weather impacts takeoff, landing, and climb performance. The service ceiling maximum altitude ensures adaptability to various environmental factors. Turbocharged models using TSIO-520 engines enhance performance in challenging conditions, maintaining consistent operation across a wide range of altitudes and temperatures.

The performance of the Cessna 310 is renowned for its speed, range, and versatility. The maximum speed of the Cessna 310 reaches 220 mph (354.064 km/h), with a cruise speed ranging from 183 to over 190 knots (338.916 km/h to 351.88 km/h) depending on engine configurations. The aircraft's range extends up to 1,000 miles (1,609 kilometers), enabled by a fuel capacity optimized for long-distance travel. Equipped with Continental O-470 engines delivering 260 horsepower (194 kilowatts) each, or optionally TSIO-520 engines producing 285 horsepower (213 kilowatts), the Cessna 310 achieves a service ceiling of 20,000 feet (6,096 meters). The rate of climb exceeds 1,600 feet (487.68 meters) per minute allows for efficient ascent capabilities.

What is the takeoff distance of a Cessna 310?

The takeoff distance of a Cessna 310 is 1,770 ft (540 m) to clear a 50-ft (15 m) obstacle at gross weight under standard conditions. The ground roll distance required for the Cessna 310 is 1,335 ft (407 meters) under standard conditions at gross weight. The total takeoff distance includes both the ground roll and the distance needed to climb to an altitude of 50 ft (15.24 m) above the runway. Some sources list a takeoff distance of 1,662 ft (506.57 m), which refers to a balanced field length or a different operational configuration. Values like 1,451 ft (442.27 m), 1,385 ft (422.15 m), or 800 ft (243.84 m) do not match standard published figures for the Cessna 310 at gross weight. Training programs use the Cessna 310 for instruction due to its reliability and versatility in various flight conditions.

The standard ground roll distance for the Cessna 310 under gross weight and standard conditions is 1,335 ft (407 m). This value represents the distance required for the aircraft to achieve liftoff without additional climb performance. Some sources cite a ground roll of 800 ft (243.84 m), which does not align with official published data for the Cessna 310 at gross weight. Such discrepancies arise from non-standard conditions or incomplete reporting of operational factors.

The total takeoff distance required for the Cessna 310 to clear a 50-ft (15 m) obstacle at gross weight is 1,770 ft (540 m). Variations in this figure, for example, 1,716 ft (523 m), 1,640 ft (499 m), and 1,395 ft (425 m), reflect differences in operational configurations or environmental conditions. These values highlight the significance of understanding specific scenarios when evaluating takeoff performance metrics. The Cessna 310 achieves consistent results under standard conditions, reinforcing its reliability in training and private operations.

The takeoff distance of 1,662 ft (506.57 m) mentioned in literature refers to balanced field length or alternate configurations. Balanced field length accounts for scenarios where the distance required for takeoff equals the distance needed to safely abort. This figure differs from standard takeoff distances and holds relevance in specific operational contexts.

1,451 ft (442.27 m) and 1,385 ft (422.15 m) are not verified gross weight figures for the Cessna 310. These unverified distances lack alignment with official performance data and cannot be relied upon for accurate calculations. Training programs and operational manuals prioritize verified metrics for safety and efficiency.



What is the engine configuration of the Cessna 310?

The Cessna 310 features two wing-mounted reciprocating piston engines, providing stability and aerodynamic efficiency. Early models are equipped with Continental O-470-B engines, each delivering 260 horsepower. Later models use Continental IO-520-M engines, providing 285 horsepower per engine. The twin-engine configuration ensures redundancy and enhanced safety during flights.

Two engines are arranged symmetrically on either wing, providing balanced thrust and better handling characteristics. This arrangement supports redundancy, allowing the aircraft to maintain flight in the event of an engine failure. The Continental O-470-B engines in early models deliver 260 horsepower, while later versions feature Continental IO-520-M engines producing 285 horsepower. Reciprocating piston engines engine type power the aircraft, utilizing a piston mechanism where pistons move within cylinders to generate rotational energy via a crankshaft.

Wing-mounted engine setup enhances aerodynamic efficiency and stability. The installation method involves attaching each engine securely under the wings using a robust mounting system. This design minimizes drag and ensures optimal airflow around the nacelles. Wing-mounted engines contribute to a stable and balanced flight experience, making the Cessna 310 suitable for long-distance travel.

Continental O-470 variants provide consistent power output across early versions, while Continental IO-520-M engines enhance performance in later iterations. Design characteristics emphasize reliability and efficiency, guaranteeing dependable operation in varied flying conditions and contributing to Cessna 310’s popularity among private pilots and commercial operators.



Cessna 310 Engine

What are the differences between a Cessna 310 and a Cessna 340?

Differences between a Cessna 310 and a Cessna 340 are explained in the table below.

Category

Cessna 310

Cessna 340

Airframe Design

Non-pressurized

Pressurized with structural reinforcements

Cabin Configuration

Standard seating layout

Club seating for improved passenger comfort

Engine Performance

260 horsepower (each)

310 horsepower (each), turbocharged engines

Maximum Cruise Speed

200-220 knots

Similar speeds, optimized for higher altitudes

Fuel Capacity

Smaller fuel tanks (~1000 nm range)

Larger fuel tanks (~1300 nm range)

Payload Capacity

Lower payload capacity due to weight limitations

Higher payload capacity due to structural reinforcements

Avionics Systems

Simpler avionics setup

Advanced avionics systems tailored for pressurized operations

Operational Altitude

Limited by non-pressurized design

High-altitude operations supported by turbocharged engines

Accessibility Features

Wing-mounted entry door

Airstair for improved accessibility

Range

~1,000 nautical miles

~1,300 nautical miles

Structural Modifications

Traditional wing design

Reinforced airframe and optimized aerodynamics

Engine performance differences horsepower directly impact cruising capabilities, as the Cessna 340 operates at higher altitudes with optimized fuel consumption rates. Structural modifications for altitude performance enhance the 340's suitability for long-distance flights. Wing and fuselage configuration differences and aerodynamic profile reflect the Cessna 340's optimization for pressurized operations, contributing to improved performance metrics. Instrument panels in the Cessna 340 feature components adapted for pressurized flights to ameliorate functionality and pilot experience. These technological advancements align with Cessna 340 design innovations and underscore the model's superiority in modern aviation applications.

The differences between a Cessna 310 and a Cessna 340 include airframe design, cabin configuration, engine performance, fuel capacity, payload capacity, and avionics systems.

The Cessna 310 cockpit is featured with primary flight instruments, avionics panel, engine instrumentation, navigation and communication radios, autopilot system, throttle quadrant, overhead panel switches, and flight controls. The Cessna 310 cockpit design ensures comprehensive situational awareness and operational control for pilots. Primary flight instruments include an airspeed indicator displaying airspeed in knots, an altimeter showing altitude in feet, and an attitude indicator providing pitch and bank angles. The avionics panel features a Horizontal Situation Indicator for navigation and communication radios like Garmin or King transceivers. Engine instrumentation monitors key parameters including RPM, oil pressure in psi, and cylinder head temperature. Navigation radios integrate VOR and ILS receivers while the autopilot system offers heading, altitude, and navigation tracking modes.

The engine instrumentation rpm gauge displays engine revolutions per minute, allowing the Cessna 310 pilot monitors engine performance within safe limits. The engine instrumentation oil pressure gauge provides readings in pounds per square inch, maintaining values between 40 and 80 psi for optimal operation. The engine instrumentation temperature gauge tracks cylinder head and oil temperatures, upgraded by advanced monitoring systems like the JPI EDM 760. Navigation radios VOR receiver integrates VHF omnidirectional range signals, enabling precise en-route navigation. Navigation radios ILS receiver delivers instrument landing system guidance during approach phases. Communication radio transceiver facilitates clear VHF communication with air traffic control and other aircraft.

The autopilot system control module engages and manages functions, including heading, altitude, and navigation tracking, assisting the Cessna 310 pilot during long flights. The autopilot system interface panel allows interaction with modes including heading bug, altitude hold, and navigation coupling. The throttle quadrant throttle lever adjusts engine power output for each engine, maintaining balanced performance. The throttle quadrant propeller control modifies propeller pitch to optimize efficiency. The throttle quadrant mixture control regulates the fuel-air mixture for optimal engine operation.

Overhead panel switches manage auxiliary systems: landing lights, strobes, pitot heat, cabin lights, and avionics master. Overhead panel indicators display status information for battery, alternator, and vacuum systems. Control yoke flight controls manipulate aileron and elevator surfaces for roll and pitch adjustments. Pedal controls rudder pedals govern the rudder for yaw control and assist in ground steering. The Cessna 310 cockpit design ensures comprehensive situational awareness and operational control for pilots through its organized layout and robust redundancy.



Where to find Cessna 310 for sale?

To find a Cessna 310 for sale, explore aircraft sales websites, aviation classifieds, and dealerships. Aircraft sales websites like Trade-A-Plane list up to 35 Cessna 310 series aircraft with prices ranging from $79,000 to $299,000. Aviation classifieds, for example, Barnstormers provide detailed advertisements, including a 1977 Cessna 310R Bearcat priced at $229,900. Aircraft dealerships offer verified inventory and dealer certification for reliable transactions. Aircraft brokerages connect buyers with a wide network of brokers who assist in negotiations and market analysis. Online aviation marketplaces feature advanced search filters and user reviews to streamline the buying process.

Aircraft dealerships’ dealer certification provides additional assurance regarding the aircraft's history and condition. Dealer certification involves rigorous inspections and adherence to maintenance protocols. Buyers benefit from direct access to certified professionals who guide them through the purchasing process. Aircraft brokerages’ broker network access connects buyers with experienced brokers familiar with the Cessna 310 market. Aircraft brokerages negotiation services assist buyers in securing favorable terms during transactions. Brokers leverage their extensive knowledge of market trends to facilitate efficient negotiations.

Online aviation marketplaces advanced search filters allow buyers to refine searches based on specific criteria: price, year, and technical specifications. Advanced search filters narrow down listings to match buyer preferences. Online aviation marketplaces user reviews offer beneficial insights into the reliability of sellers and brokers. User reviews detail past experiences, helping buyers avoid potential issues. Aircraft auction houses’ auction schedules provide dates for upcoming auctions featuring models like the Cessna 310. Competitive bidding platforms at these auctions enable buyers to participate in real-time bidding. Aircraft auction houses’ bid history offers data on past transactions, aiding buyers in understanding market dynamics and making informed decisions.

Maintenance history shows aircraft's service records and details about repairs, overhauls, and routine checks. Used aircraft listings price history tracks fluctuations in the aircraft's value over time. Price history helps buyers assess whether the asking price aligns with market trends. Reliability and capacity to carry multiple passengers make the Cessna 310 a popular choice among private pilots and small businesses. Models like the Riley Rocket modification enhance performance and speed, appealing to buyers seeking upgraded capabilities.



What is the cost of a Cessna 310?

The cost of a Cessna 310 varies based on factors like the model year, condition, upgrades, and flight hours. A pre-owned Cessna 310Q in average condition costs around $100,000. Prices for fully upgraded models reach $400,000 due to advanced avionics and engine modifications. Aircraft requiring restoration or salvage are priced at $60,000 and $20,000 respectively. High flight hours reduce the value, with some models priced at $80,000. Custom-modified versions of the Cessna 310 cost around $500,000, reflecting extensive modernization efforts.

The Cessna 310Q in average condition costs around $120,000, while models with high flight hours are priced at $80,000. Pre-owned Cessna 310s with low flight hours command a premium, reaching $350,000 due to their reduced wear and extended operational lifespan. Fully upgraded versions of the Cessna 310, equipped with modern avionics and engine enhancements, are valued at $400,000, reflecting the investment in technological improvements.

Aircraft requiring restoration are available for $60,000, appealing to buyers focused on rebuilding projects. Salvage title Cessna 310s repairable for $20,000 offer an affordable entry point for those capable of extensive repairs. Damaged models needing engine replacement are priced at $15,000, emphasizing the cost implications of mechanical issues.

Custom-modified versions of the Cessna 310 reach $500,000, driven by comprehensive modernization efforts that include advanced systems and interior upgrades. Rare limited-edition models, although not currently in production, carry a price tag of $250,000, highlighting their exclusivity and appeal to collectors or enthusiasts seeking unique aircraft.

Flight hours influence the Cessna 310 cost, with lower hours increasing value and higher hours reducing it. Condition, age, and the presence of upgrades further contribute to cost variability across all categories. Rarity influences pricing for custom builds and limited-edition configurations, which elevate the Cessna 310 price beyond standard pre-owned models.