O 520 Series
The O 520 Series encompasses a range of robust aircraft engines designed for general aviation applications. These horizontally opposed, six-cylinder piston engines are renowned for their reliability, durability, and consistent performance, making them a popular choice for a variety of aircraft, including training aircraft, personal transport planes, and light utility aircraft. Their design prioritizes efficient operation and longevity, contributing significantly to the operational safety and economic viability of aircraft equipped with them.
Comprehensive technical documentation is available for the O 520 Series, providing essential information for owners, maintenance personnel, and technicians. This documentation includes detailed maintenance manuals outlining routine service schedules...
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This manual covers the Cessna 210 Centurion Series aircraft, produced between 1970 and 1975 by the Cessna Aircraft Company. These aircraft are recognized for their robust engineering and reliability, offering a versatile platform for various aviation needs. Notable features include the 6-seat configuration in the 210K model and aerodynamic improvements in the 210L series that enhance cruise speed. Engine options for these models include the Continental IO-520-L, and for the 210L, the TSIO-520-L, with the 1970 210K model boasting 300 hp. The 210L features a 24-volt electrical system and an electrical pump replacing the engine-driven hydraulic pump, contributing to its operational efficiency.
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This manual covers the aircraft manufactured between 1970 and 1973. These aircraft are known for their robust engineering and reliability, offering a spacious cabin with seating for up to six occupants and featuring an enlarged cabin with a single rear side window. Powered by engines such as the Continental IO-520-L producing 300 hp, these models were designed for efficient travel, with aerodynamic enhancements contributing to an approximate 8-knot increase in cruise speed. The electrical system operates on 24 volts and utilizes an electrical pump for hydraulic functions.
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This manual covers the aircraft manufactured between 1970 and 1973. Known for its robust engineering and reliability, the series offers advanced features designed for efficient and comfortable air travel. This particular generation of aircraft benefited from aerodynamic improvements, contributing to enhanced cruise speeds, and was typically equipped with a powerful Continental IO-520-L engine.
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This manual covers the Cessna 210 Centurion Series aircraft manufactured between 1970 and 1976. These aircraft are known for their robust engineering and reliability, offering a versatile platform for various aviation needs. The Centurion Series typically features a 6-seat configuration and is powered by Continental engines ranging from 285 to 310 horsepower, with fuel capacities of 90 US gallons and takeoff weights of up to 3,800 lb for models from 1970 onwards. This manual provides essential information for understanding and maintaining these aircraft.
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The Cessna 210 Centurion, produced between 1970 and 1976, is a distinguished high-wing monoplane renowned for its robust engineering and reliable performance. This versatile aircraft, capable of seating up to six occupants, features a retractable tricycle landing gear system and is powered by a reciprocating engine from Continental Motors, typically delivering 260 horsepower. With its substantial wingspan and a maximum takeoff weight of approximately 1520 kg, the 210 Centurion is engineered for a wide range of aviation applications, embodying a commitment to quality and operational efficiency.
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The Continental TS10-520 is a turbosupercharged, fuel-injected, opposed piston aircraft engine designed for aviation applications. With a displacement of 520 cubic inches, this air-cooled engine is engineered for reliability and performance in demanding flight conditions. It utilizes Aviation Gasoline (Avgas) and is a product of Continental's commitment to quality in aircraft propulsion systems. This manual covers various models including the TSIO-520-4, TSIO-520-G, TSIO-520-H, TSIO-520-M, TSIO-520-P, TSIO-520-R, TSIO-520-T, L/TS IO-520AE, TSIO-520-AF, and TSIO-520-CE.
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This manual covers the Continental TSIO-520 aircraft engine, manufactured by Continental Aerospace Technologies. This turbocharged, fuel-injected, horizontally opposed engine, with a displacement of 520 cubic inches, is designed for demanding aviation applications. Its robust engineering ensures reliability and performance, making it a trusted choice for pilots and aircraft operators.
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This manual covers the Continental TSIO-520 Series, a line of turbocharged, fuel-injected aircraft engines renowned for their robust engineering and reliability in demanding aviation applications. Designed for optimal performance and longevity, these engines represent a significant advancement in aircraft propulsion, offering dependable power for a variety of aircraft. The quality and precision inherent in the Continental TSIO-520 Series ensure that operators receive exceptional value and operational confidence.
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This manual covers the TSIO-520 Series aircraft engines, specifically designed for overhaul and service repair. The TSIO-520 engine family is renowned for its robust engineering and reliability, making it a trusted component in aviation. This comprehensive guide addresses various models within the series, including the TSIO-520-L, LB, WB, M, N, P, R, BB, DB, EB, JB, KB, LB, NB, UB, VB, T, U, UB, and VB, ensuring detailed support for a wide range of applications.
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This manual covers the Continental Motors X30628A, an aircraft engine from the IO-520 Series, designed for aviation propulsion. It details parts for variants A, D, E, F, J, K, and L, utilizing Aviation Gasoline (Avgas). This Illustrated Parts Catalog (IPC) provides essential information for identifying and managing components of this robust engine.
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The Continental Aircraft Engines IO-520 is a renowned horizontally opposed, air-cooled, fuel-injected aircraft engine, designed for reliable aircraft propulsion. With a displacement of 520 cubic inches and horsepower ratings that vary by specific model, such as 285 HP or 300 HP, the IO-520 series is known for its robust engineering and performance in demanding aviation applications. This engine series utilizes Aviation Gasoline (Avgas) and is engineered for efficiency and durability in flight.
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This manual covers the Continental IO-520-BB aircraft engine, manufactured by Continental Aircraft Engines. This horizontally opposed, air-cooled, naturally aspirated engine, with a displacement of 520 cubic inches, is designed for aviation applications and utilizes aviation gasoline. Its robust engineering ensures reliability for demanding flight operations.
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The Continental IO-520 is a robust aircraft engine designed for propulsion, featuring a horizontally opposed, air-cooled, fuel-injected configuration. This six-cylinder engine, with a displacement of 520 cubic inches, utilizes Aviation Gasoline (Avgas) and is equipped with a dual magneto and dual spark plug ignition system. Engineered for reliability and performance under varying ambient temperature and pressure conditions, the IO-520 represents a significant contribution to aircraft operations, built with a commitment to engineering excellence.
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The Continental IO-520 Series aircraft engine is a horizontally opposed, six-cylinder, air-cooled powerplant with a displacement of 520 cubic inches, designed for demanding aviation applications. Engineered for reliability and performance, this engine utilizes Aviation Gasoline (Avgas) and represents a robust solution for aircraft requiring dependable power. Its construction emphasizes durability and efficiency, making it a trusted component in various aircraft models.
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The Continental GTSIO-520 is a powerful and reliable aircraft engine, designed for demanding aviation applications. This horizontally opposed, six-cylinder, turbocharged, and fuel-injected engine boasts 520 cubic inches of displacement and is air-cooled for optimal performance. Engineered for precision and durability, the GTSIO-520 is built to provide consistent power output and dependable operation in a variety of flight conditions, making it a preferred choice for aircraft propulsion.
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This manual covers the Continental IO-520 aircraft engine, manufactured by Continental Motors Group. The IO-520 is a horizontally opposed, 6-cylinder, air-cooled, fuel-injected engine with a displacement of 520 cubic inches, producing 285 horsepower at 2700 RPM. Designed for propeller-driven aircraft propulsion, this engine is known for its robust engineering and reliability in demanding aviation applications. Its specifications include a bore of 4.625 inches, a stroke of 4.500 inches, and a compression ratio of 7.0:1, with a dry weight of approximately 370 lbs. The engine utilizes Aviation Gasoline (Avgas) and requires an 8-quart oil capacity.
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This Illustrated Parts Catalog (IPC) pertains to Continental Aerospace Technologies' GTSIO-520 series aircraft engines, specifically covering models GTSIO-520 C, D, F, and K. Designed for the identification and ordering of replacement parts, this catalog is an essential resource for maintaining the operational integrity of these engines. The GTSIO-520 series represents a significant contribution to aviation powerplants, known for their robust engineering and reliability in demanding flight conditions.
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This manual pertains to the Continental TSIO-520 series aircraft engines, a line of horizontally opposed, air-cooled, turbocharged, and fuel-injected powerplants designed for aviation applications. With a displacement of 520 cubic inches and a typical power output ranging from 285 to 325 horsepower, these engines are recognized for their robust engineering and reliability in demanding flight conditions. This parts catalog focuses on the components and assemblies essential for maintaining the operational integrity of the TSIO-520 engine family.
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This document pertains to the Continental TSIO-520-BE aircraft engine, manufactured by Continental Aerospace Technologies. Produced in 1984, this turbocharged, fuel-injected, opposed piston engine offers 520 cubic inches of displacement and is designed for propulsion in general aviation aircraft. Its robust engineering ensures reliable performance, making it a trusted component for aviation operations. This parts catalog, identified by part number X30576A, provides essential information for maintaining this specific engine model.
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This manual covers the Continental IO-520 Series aircraft engines, a line of engines renowned for their robust engineering and reliability in aviation applications. Designed for the demanding requirements of aircraft servicing and repair, the IO-520 series represents a commitment to performance and durability. This comprehensive guide is intended to support owners and operators in maintaining these engines to the highest standards.
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This document provides essential information for the Continental TSIO-520 SANDCAST Series aircraft engines, encompassing various models including the TSIO-520-C, G, H, M, P, R, T, AF, L/T-AE, and CE. These horizontally opposed, six-cylinder, air-cooled, fuel-injected, and turbocharged engines are designed for aviation propulsion and utilize Aviation Gasoline (Avgas). Known for their robust engineering, these engines are a critical component in many aircraft, delivering reliable performance for demanding flight operations.
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This manual pertains to the Continental TSIO-520 Permold, an aircraft engine designed for reliable performance and identified by its robust engineering. This catalog provides detailed information for replacement parts and identification, ensuring that operators can maintain the integrity and functionality of their aircraft's propulsion system. The TSIO-520 Permold engine is engineered for demanding aviation applications, utilizing Aviation Gasoline (Avgas) to deliver consistent power.
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This manual covers the Continental Motors IO-520 Permold Series aircraft engine, designed for aviation applications. The IO-520 engine is a 6-cylinder, horizontally opposed, air-cooled, normally aspirated unit with a displacement of 520 cubic inches and a power output of 285 horsepower, utilizing Aviation Gasoline (Avgas). This engine series, including models IO-520-B, IO-520-BA, IO-520-BB, IO-520-C, IO-520-CB, IO-520-M, and IO-520-MB, is recognized for its robust engineering and reliable performance in demanding flight environments.
