Lycoming O 360 Series
The O-360 series encompasses a range of horizontally opposed, four-cylinder aircraft engines manufactured by Lycoming. These engines are widely recognized for their reliability, robust performance, and versatility, making them a popular choice for a variety of general aviation aircraft. Applications include training aircraft, personal transportation planes, and some aerobatic models, where their power output and durability are essential for safe and effective operation. The O-360 series is characterized by its air-cooled design and consistent power delivery across its operational envelope.
Comprehensive documentation is available for the O-360 series, including detailed maintenance manuals, overhaul instructions, and troubleshooting guides. These resources provide essential...
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The Cessna 177 Cardinal, produced between 1968 and 1977, represents a significant advancement in general aviation aircraft design. Engineered for reliability and performance, this aircraft is powered by a Lycoming O-360-A1F6D engine delivering 180 horsepower, enabling a maximum speed of 136 knots and a range of 604 nautical miles. Its spacious cabin accommodates one pilot and three passengers, making it suitable for a variety of missions including travel, personal use, and flight training. The Cardinal is recognized for its comfortable ride and stable flight characteristics, reflecting Cessna's commitment to quality and pilot satisfaction.
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The Cessna 177 Cardinal, produced between 1968 and 1977, is a versatile aircraft powered by a Lycoming O-360-A1F6D engine delivering 180 horsepower. This model features a flat-4 engine configuration, a wingspan of 35 feet 6 inches, and a length of 27 feet 8 inches. Designed for one pilot and up to three passengers, the Cardinal offers a maximum speed of 136 knots and a service ceiling of 14,600 feet, making it suitable for a range of general aviation missions. Its robust engineering and reliable performance have made it a respected aircraft in its class.
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The Cessna 177 Cardinal, produced between 1969 and 1976, is an aircraft designed for a variety of aviation needs, including repair, service, restoration, maintenance, rebuilding, and diagnostics. This model is powered by a Lycoming O-360-A1F6D flat-4 engine, delivering 180 horsepower, and is capable of a maximum speed of 157 mph. Its robust engineering ensures reliability for its intended uses, making it a dependable platform for pilots and aviation professionals.
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The Lycoming IO-360 M1A, a 2008 model aircraft engine, represents a pinnacle of aviation propulsion engineering. Manufactured by Lycoming Engines, this horizontally opposed, air-cooled, fuel-injected powerplant delivers 180 horsepower at 2700 RPM. With a displacement of 360 cubic inches and designed for aviation gasoline, the IO-360 M1A is renowned for its reliability and robust performance, making it a trusted choice for demanding flight operations. Its meticulous design ensures consistent power output and operational efficiency.
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The Lycoming 0-360 and H0-360 series aircraft engines are renowned for their robust design and reliable performance in aviation propulsion. These horizontally opposed engines, with a displacement of 360 cubic inches, are engineered to operate on Aviation Gasoline (Avgas) and are a staple in numerous aircraft applications. Their reputation for quality engineering ensures consistent power delivery and operational longevity, making them a trusted choice for pilots and aircraft manufacturers alike.
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This manual pertains to the O-360 and O-540 series aircraft engines. These engines are known for their horizontally opposed, air-cooled configurations, with the O-360 featuring four cylinders and a displacement of 360 cubic inches, while the O-540 is a six-cylinder engine with a displacement of 540 cubic inches. They are engineered for reliable performance in aviation applications.
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This manual covers Lycoming IO-360 Series, LIO-360 Series, HIO-360 Series, TIO-360 Series, and AEIO-360 Series aircraft engines, specifically those with wide cylinder flange models. These horizontally opposed, air-cooled piston engines are renowned for their robust engineering and reliability in aviation applications. This Illustrated Parts Catalog (IPC) is designed to assist in the precise identification and ordering of components for these engine variants, ensuring continued operational integrity and performance.
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This manual pertains to the Lycoming TO-360 Series aircraft engines, manufactured by Textron Lycoming. These engines are engineered for reliable operation and are intended for use in aircraft where their performance and durability are critical. The TO-360 Series represents a commitment to quality in aviation propulsion, designed to meet the demanding requirements of pilots and maintenance personnel.
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This manual covers the Lycoming O, IO, HO, HIO-360 series aircraft engines with standard cylinder flanges. These engines are known for their robust engineering and reliability, making them a cornerstone in aviation. This parts catalog manual is designed to assist in the procurement and servicing of all components for these specific Lycoming engine models, ensuring operational integrity and longevity.
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This parts catalog covers the IO-360 B1G6, a horizontally opposed, 4-cylinder, air-cooled aircraft engine designed for aviation applications. With a displacement of 380 cubic inches and utilizing Aviation Gasoline (Avgas), this engine is engineered for reliability and performance in demanding flight environments. Its robust construction and proven design make it a cornerstone for various aircraft, reflecting a commitment to quality in aviation propulsion systems.
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This manual pertains to the Lycoming IO-360 PC-106 aircraft engine, manufactured by Avco. This fuel-injected, horizontally opposed engine features 360 cubic inches of displacement and a six-cylinder configuration. Designed for aviation applications, it is known for its robust engineering and reliability. This Illustrated Parts Catalog (IPC) is an essential resource for identifying and ordering components for various compatible engine models, including O, HO, and HIO variants.
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This manual covers the Textron Lycoming IO-360-B1G6 aircraft engine, a fuel-injected, horizontally opposed engine with a displacement of 360 cubic inches. Designed for wide cylinder flange crankcase model aircraft engines, this component is built with Textron Lycoming's renowned engineering quality and reliability. Its robust design ensures consistent performance for a variety of aviation applications.
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This manual covers the Lycoming IO-360-L2A aircraft engine, a horizontally opposed, 4-cylinder, air-cooled engine designed for aviation applications. With a displacement of 360 cubic inches and an output of 180 horsepower, this engine is engineered for reliability and performance in demanding flight conditions. It utilizes Aviation Gasoline (Avgas) and represents a significant component in the Lycoming Engines product line, known for its robust construction and consistent operation.
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This manual pertains to the Textron Lycoming IO-360-M1A Wide Cylinder Flange Model aircraft engine crankcase. Manufactured by Textron Lycoming, this engine is designed for aviation applications, specifically for identifying replacement parts essential for the assembly and maintenance of the IO-360-M1A wide cylinder flange model. The product category is Aircraft Engine Parts Catalog, indicating its focus on component identification and procurement.
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The Textron Lycoming O, LO, TO -360 Series Wide Cylinder Flange Model aircraft engines are engineered for reliable performance in aviation applications. This series, encompassing Opposed (O), Fuel Injected (LO), and Turbocharged Opposed (TO) configurations, represents a commitment to robust design and operational excellence within the -360 engine model series. The specific focus on the Wide Cylinder Flange Model ensures precise compatibility and optimal function for these critical components.
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This Parts Catalog Manual covers Lycoming TO-360 & LTO-360 Series Aircraft Engines. Designed for the identification, procurement, and servicing of parts, this manual is an essential resource for maintaining the integrity and performance of these aircraft engines. Lycoming engines are renowned for their robust engineering and reliability, making this catalog indispensable for ensuring continued operational excellence.
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This operator manual covers the Textron Lycoming O-360, HO-360, IO-360, AIO-360, HIO-360, and TIO-360 series aircraft engines. These horizontally opposed piston engines are designed for aviation applications and utilize Aviation Gasoline (Avgas). The manual, with serial number 60297-12, is presented in English and is 177 pages long, designed to be bookmarked and searchable for ease of use.
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This Illustrated Parts Catalog (PC-306-5) provides a comprehensive listing of parts for the Textron Lycoming O-360, LO-360-A1H6 Wide Cylinder Flange Crankcase model aircraft engines. Designed for clarity, this catalog is written to be easily understood by a wide range of users. Its digital format includes bookmarking for quick navigation and search functionality, allowing users to efficiently locate specific information.
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This manual pertains to the O-360-2JA, an aircraft engine designed for applications requiring a wide cylinder flange crankcase. As an Opposed (O-series) engine, the O-360-2JA is part of the established O-360 engine family, known for its robust engineering and reliability in aviation. This Illustrated Parts Catalog (IPL), provides comprehensive details for this specific variant, ensuring precise identification and management of its components.
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This illustrated parts catalog provides comprehensive information for the Textron Lycoming O-360-A1P aircraft engine. Designed for model aircraft engines, this horizontally opposed, naturally aspirated engine features a 360 cubic inch displacement and a wide cylinder flange crankcase. Textron Lycoming is recognized for its commitment to engineering quality and reliability, ensuring the performance and longevity of its aircraft engine components.
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This manual covers the O-360-A4N, a horizontally opposed, 4-cylinder aircraft engine with a displacement of 360 cubic inches. Designed for wide cylinder flange crankcase model aircraft, this engine is renowned for its robust engineering and reliable performance in aviation applications. Its construction emphasizes durability and efficiency, making it a trusted choice for demanding flight operations.
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This manual covers the Textron Lycoming O-360-B2C, a reciprocating aircraft engine with a displacement of 360 cubic inches. Designed for wide cylinder flange crankcase model aircraft engines, this component is engineered for reliability and performance in aviation applications. Its robust construction and precise manufacturing ensure dependable operation, making it a trusted choice for aircraft operators and maintenance professionals.
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This manual pertains to the Lycoming O-360-C1G aircraft engine, manufactured by Textron Lycoming. Designed for model aircraft engines, this component features a wide cylinder flange crankcase and a nominal displacement of 360 cubic inches. The engineering quality and reliability inherent in Textron Lycoming products ensure consistent performance and durability for its intended applications.
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This document pertains to the Textron Lycoming O-360-C4F and O-360-C4P aircraft engines, part of the O-360 Series. These opposed, naturally aspirated, air-cooled piston engines displace 360 cubic inches and are designed for use with aviation gasoline. They feature a wide cylinder flange crankcase, contributing to their robust engineering and reliability for aviation applications. This Illustrated Parts Catalog (IPC), manual number PC-306-8, provides detailed information for these specific engine models.
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This manual covers the Lycoming O-360-L2A, an opposed, 4-cylinder, air-cooled aircraft engine designed for model aircraft engines. Featuring a wide cylinder flange and a displacement of 360 cubic inches, this engine is engineered for reliability and performance. Its robust construction and precise manufacturing ensure dependable operation, making it a preferred choice for enthusiasts and builders alike.
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This manual covers the O-360-A4P, an aircraft engine designed for wide cylinder flange crankcase applications. This engine is part of the O-360 Series and is recognized for its reliability and engineering quality. This Illustrated Parts Catalog (IPC) provides detailed information essential for the maintenance and support of these robust aircraft engines.
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This manual covers the Avco Lycoming TIO-360-C1A6D, an aircraft engine featuring a wide cylinder flange design and a displacement of 360 cubic inches. Manufactured by Avco Lycoming, this engine is engineered for aviation applications, emphasizing reliability and performance. The illustrated parts catalog provides comprehensive details for this specific model, ensuring users have access to precise information for parts identification and management.
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The Textron Lycoming IO-360 M1A Wide Cylinder is a robust aircraft engine designed for reliable propulsion in aviation applications. This fuel-injected, air-cooled, horizontally opposed piston engine boasts a displacement of 360 cubic inches and features a wide cylinder flange crankcase. Engineered for demanding flight conditions, it utilizes Aviation Gasoline (Avgas) and represents a significant contribution to aviation technology through its quality and performance.
