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Lycoming IO-360-L2A Aircraft Engine 180-220 HP

Lycoming IO-360-L2A Aircraft Engine 180-220 HP
Lycoming IO-360-L2A Aircraft Engine 180-220 HP
Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP Lycoming IO-360-L2A Aircraft Engine 180-220 HP
Podstawowe informacje
Miejsce pochodzenia: Ameryka
Nazwa handlowa: Lycoming
Orzecznictwo: FAA 8130-3
Numer modelu: IO-360-L2A
Minimalne zamówienie: 1 ea
Zasady płatności: , T/t
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Lycoming IO-360-L2A Engine

Lycoming IO-360-L2A Aircraft Engine 180-220 HP
The Lycoming IO-360-L2A engine occupies an important position in the field of light general aircraft with its excellent performance, reliability and easy maintenance, and has become the preferred power source for many pilots and aviation enthusiasts.
Part Numbers
New Rebuilt Overhaul
ENPL-RT9543 RENPL-RT9543 HENPL-RT9543
ENPL-RT9918 RENPL-RT9918 HENPL-RT9918
ENPL-RT10230 RENPL-RT10230 HENPL-RT10230
ENPL-RT10437 RENPL-RT10437 HENPL-RT10437
ENPL-RT10596 RENPL-RT10596 HENPL-RT10596
Basic Information
  • Type: Four-cylinder, direct drive, horizontally opposed, air-cooled.
  • Cylinder structure: Conventional air-cooled structure, the cylinder head is cast from aluminum alloy, and the combustion chamber is precision machined. The rocker shaft bearing support is cast integrally with the head, with a shell forming the rocker box. The cylinder barrel has deep integrated cooling fins, and the interior is ground and polished.
  • Fuel system: Equipped with a fuel injection system that can adjust the fuel flow according to the air flow ratio, and the fuel is vaporized at the intake port.
  • Turbocharger: The TIO-360 series is equipped with a turbocharger that provides a constant air density to the fuel injector inlet from sea level to critical altitude.
Performance Parameters
  • Power output: The power of the IO-360 engine varies from model to model, and generally ranges between 180 hp and 220 hp.
  • Speed: The maximum continuous speed is typically 2700 to 2800 rpm, depending on the specific model and usage conditions.
  • Efficiency: High fuel efficiency with approximately 11 to 14 miles per gallon in cruise mode. Specific fuel consumption varies based on aircraft model, weight, and flight conditions.
Application Fields
  • General aviation: Widely used in light general aircraft such as Cessna 172 and Piper Archer for private flights, flight training, and sightseeing.
  • Aerospace sports: Used as a power source for powered paragliders, delta wings, and other aircraft due to its reliability and stable performance.
Advantages and Features
  • High reliability: Full authority digital engine control (FADEC) system automatically monitors and adjusts engine parameters to ensure optimal performance and safety.
  • Easy maintenance: Simple structural design facilitates daily maintenance. Lycoming provides comprehensive maintenance manuals and technical support.
  • Long service life: Durable design with a service life of thousands of hours under normal use and maintenance.
Contact us for prices.

Etykietka:

Lycoming Electronic Ignition System,

Lycoming Aircraft Piston Engine,

Piper Aircraft Engine

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