Continental O-240
The Continental O-240 engine is a four-cylinder, horizontally opposed, air-cooled aircraft engine that was developed in the late 1960s for use in light aircraft by Continental Motors, Inc. The first O-240 was certified on 7 July 1971.
Continental CO-240-AContinental IO-240Continental IO-240-AContinental IO-240-BContinental IOF-240Continental IOF-240-BContinental O-240-ARolls-Royce/Continental O-240Rolls-Royce/Continental O-240-ARolls-Royce Continental O-240Rolls-Royce Continental O-240-ATeledyne Continental Motors IO-240-ATeledyne Continental Motors IO-240-BTeledyne Continental Motors IO-240F
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Continental O-240
The Continental O-240 engine is a four-cylinder, horizontally opposed, air-cooled aircraft engine that was developed in the late 1960s for use in light aircraft by Continental Motors, Inc. The first O-240 was certified on 7 July 1971.
has abstract
Der Continental O-240 ist ein ...... 7. Juli 1971 musterzugelassen.
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The Continental O-240 engine i ...... was certified on 7 July 1971.
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bore
compression
coolingsystem
Air-cooled
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developed from
displacement
first run
fuelsystem
Aerosance FADEC system
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fueltype
major applications
manufacturer
national origin
United States
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power/weight
ref
TYPE CERTIFICATE DATA SHEET NO. E7SO
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specpower
stroke
type
valvetrain
One intake and one exhaust valve per cylinder
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weight
wikiPageUsesTemplate
comment
Der Continental O-240 ist ein ...... 7. Juli 1971 musterzugelassen.
@de
The Continental O-240 engine i ...... was certified on 7 July 1971.
@en
label
Continental O-240
@de
Continental O-240
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