Lycoming O-435

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O-435
Motore aeronautico - Museo scienza tecnologia Milano D0672.jpg
Type Piston tank and aircraft engine
National origin United States
Manufacturer Lycoming Engines
First run 1939
Major applications Beechcraft Bonanza
Bell 47
Helio Courier
Hiller OH-23 Raven
M22 Locust
Stinson L-5 Sentinel
Produced 1942–1975 out of production
Developed from Lycoming O-290

The Lycoming O-435 is an American 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.

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-435-6
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
270 hp (201 kW)
TVO-435-A
TVO-435-25
260 hp (194 kW)
VO-435
200 hp (149 kW)
VO-435-23
250 hp (186 kW)
VO-435-B1B

Applications[]

A Lycoming TVO-435 installed in a Bell 47G
Aircraft
Other

Specifications (O-435-D)[]

Data from Jane's.[1]

General characteristics

  • Type: Six-cylinder horizontally-opposed gasoline piston engine
  • Bore: 4.875 in (123.8 mm)
  • Stroke: 3.875 in (98.4 mm)
  • Displacement: 434 cu in (7.1 L)
  • Width: 33.5 in (851 mm)
  • Height: 43.5 in (1,105 mm)
  • Dry weight: 433 lb (196.6 kg)

Components

  • Valvetrain: Overhead valve (OHV, pushrod actuated), 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 (helicopter installations)
  • Reduction gear: Direct-drive

Performance

See also[]

Related development

Comparable engines

Related lists

References[]

Notes[]

  1. ^ Bridgman 1994, p. 78d.

Bibliography[]

  • Bridgman, Leonard. Jane's All the World's Aircraft 1945-46. Hammersmith, London: HarperCollinsPublishers (1994 reprint). ISBN 000 470831-8

External links[]

Media related to Lycoming O-435 at Wikimedia Commons

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