Continental O-300

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O-300
Rolls-Royce Continental O-300.JPG
Rolls-Royce Continental O-300 on display at the Solent Sky museum, England.
Type Piston aircraft engine
National originUnited States
Manufacturer Continental Motors
Major applications
Manufactured1947–present
Developed from Continental C-125

The Continental O-300 and the C145 are a family of air-cooled flat-6 aircraft piston engines built by Teledyne Continental Motors. [1]

Contents

First produced in 1947, versions were still in production as of 2004. It was produced under licence in the United Kingdom by Rolls-Royce in the 1960s.

Development

Continental O-300 engine installation in a Cessna 172 Field maintenance on a 1956 model Cessna 172.JPG
Continental O-300 engine installation in a Cessna 172

The C-145 was developed from the 125 hp (93 kW) C-125 engine. Both powerplants share the same crankcase, although the C-145 produces an additional 20 hp (15 kW) through a longer piston stroke, higher compression ratio of 7.0:1 and different carburetor jetting. [1]

The O-300 is a modernized C-145 and retains the same weight, dimensions, bore, stroke, compression ratio, displacement and output power of the earlier engine. [1]

GO-300

The GO-300 employs a reduction gearbox, so that the engine turns at 3200 rpm to produce a propeller rpm of 2400. The GO-300 produces 175 hp (130 kW) whereas the ungeared O-300 produces 145 hp (108 kW). [1]

The GO-300 engine has a TBO (Time Between Overhaul) of 1200 hours, while 1800 hours is the standard for ungeared O-300 engines. The GO-300 engine suffered reliability problems as a result of pilots mishandling the engine and operating it at too low an engine rpm. This caused the Cessna Skylark to develop a poor reputation for engine reliability. Many Skylarks flying today have been converted to different, larger-displacement, direct-drive engines. [2]

Variants

C145
Six-cylinder, 145 hp (108 kW), direct-drive engine. [1]
C145-2
O-300
Modernized C145, 145 hp (108 kW), direct drive engine. [1]
O-300-A
O-300-B
O-300-C
O-300-D
O-300-E
Limited production for the Beagle B.218X twin that never went into production [3]
GO-300
Geared O-300, 175 hp (130 kW) at 3200 crankshaft rpm, 2400 propeller rpm. [1]
GO-300-A
GO-300-C
GO-300-D
Voyager 300
Liquid-cooled, fuel-injected version developing 170 hp (127 kW) at 2,700 rpm.
Rolls-Royce-Continental O-300
Licence production in the United Kingdom.

Applications

Cessna 175 showing the cowling bulge behind the propeller hub created by the GO-300 reduction gearbox Cessna175ASkylark03.jpg
Cessna 175 showing the cowling bulge behind the propeller hub created by the GO-300 reduction gearbox

O-300

GO-300

Voyager 300

Specifications (O-300)

Reference: Engines for Homebuilt Aircraft & Ultralights [1]

General characteristics

Components

Performance

See also

Related lists

References

  1. 1 2 3 4 5 6 7 8 Christy, Joe: Engines for Homebuilt Aircraft & Ultralights, pages 60-63. TAB Books, 1983. ISBN   0-8306-2347-7
  2. ↑ Perdue, Scott. "A Lark That Won't Quit". Archived from the original on 5 November 2015. Retrieved 19 December 2008.
  3. ↑ Flight Global, 21 March 1963, p. 399
  4. ↑ Murphy, Daryl (2006). "The Cessnas that got away". Archived from the original on 27 February 2009. Retrieved 22 December 2008.
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