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Lycoming O 435

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Lycoming O-435

The Lycoming O-435 is a six-cylinder, horizontally opposed fixed-wing aircraft and helicopter engine made by Lycoming Engines. The engine is a six-cylinder version of the four-cylinder Lycoming O-290.

Contents

Design and development

The powerplant is a horizontally opposed Lycoming six-cylinder design. It is a direct-drive or geared, air-cooled, and normally aspirated engine. The cylinders have steel barrels with aluminum heads, and the valves are operated by hydraulic lifters. The crankshaft is supported in an aluminum-alloy split case by four main bearings and one ball-thrust bearing, and lubricating oil is supplied from a 12 quart wet sump. The camshaft rides in journals that do not employ bearing inserts. The accessory housing supports two magnetos, a starter, a generator, and a dual tach drive. A spare mounting pad is included for a vacuum pump.

Variants

All engines have an additional prefix preceding the 435 to indicate the specific configuration of the engine. There are also numerous engine suffixes, denoting different accessories such as different manufacturers' carburetors, or different magnetos.

XO-435-1
XO-435-3
(GO-435)
O-435-5
(O-435-B)
O-435-7
(O-435-B1)
O-435-9
O-435-11
O-435-13
O-435-A
O-435-B
O-435-C
O-435-D
GO-435
GO-435-B
TVO-435-A

Applications

Aircraft
Other
  • M22 Locust - tank
  • Specifications (O-435-D)

    Data from Jane's.

    General characteristics

  • Type: Six-cylinder horizontally-opposed gasoline piston engine
  • Bore: 4.875 in (123.7 mm)
  • Stroke: 3.875 in (98.4 mm)
  • Displacement: 434 cu in (7.1 L)
  • Width: 33.5 in (824 cm)
  • Height: 43.5 in (1,105 cm)
  • Dry weight: 433 lb (196.6 kg)
  • Components

  • Valvetrain: Overhead valve, one inlet and one exhaust valve per cylinder
  • Fuel system: Marvel-Schebler carburetor
  • Fuel type: 100 octane gasoline
  • Oil system: Pressure pump type
  • Cooling system: Air-cooled by fan
  • Reduction gear: Direct-drive
  • Performance

  • Power output: 212 hp (158 kW) at 3,000 rpm at sea level
  • Compression ratio: 7.5:1
  • References

    Lycoming O-435 Wikipedia